Explore: Wind Tunnel Tests

Discover books, insights, and more — all in one place.

Learn more about Wind Tunnel Tests with top reads curated from trusted sources — all in one place.

Topic Search

Search for any topic

AI-Generated Overview About “wind-tunnel-tests”:


Books Results

Source: The Open Library

The Open Library Search Results

Search results from The Open Library

1Hot-jet simulation in cryogenic wind tunnels

By

“Hot-jet simulation in cryogenic wind tunnels” Metadata:

  • Title: ➤  Hot-jet simulation in cryogenic wind tunnels
  • Author:
  • Language: English
  • Number of Pages: Median: 45
  • Publisher: ➤  For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
  • Publish Date:
  • Publish Location: ➤  Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]

“Hot-jet simulation in cryogenic wind tunnels” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1989
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

Online Access

Downloads Are Not Available:

The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

Online Borrowing:

    Online Marketplaces

    Find Hot-jet simulation in cryogenic wind tunnels at online marketplaces:


    2Semi-span model testing in the National Transonic Facility

    By

    “Semi-span model testing in the National Transonic Facility” Metadata:

    • Title: ➤  Semi-span model testing in the National Transonic Facility
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Washington, DC

    “Semi-span model testing in the National Transonic Facility” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1993
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

    Online Borrowing:

      Online Marketplaces

      Find Semi-span model testing in the National Transonic Facility at online marketplaces:


      3Two-dimensional converging-diverging rippled nozzles at transonic speeds

      By

      “Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:

      • Title: ➤  Two-dimensional converging-diverging rippled nozzles at transonic speeds
      • Author:
      • Language: English
      • Number of Pages: Median: 105
      • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

      “Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1994
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Access

      Downloads Are Not Available:

      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

      Online Borrowing:

        Online Marketplaces

        Find Two-dimensional converging-diverging rippled nozzles at transonic speeds at online marketplaces:


        41999 NASA High-Speed Research Program Aerodynamic Performance Workshop

        By

        “1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:

        • Title: ➤  1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
        • Author: ➤  
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va - [Springfield, Va

        “1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1999
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

        Online Borrowing:

          Online Marketplaces

          Find 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop at online marketplaces:


          5Numerical simulation of the SOFIA flowfield

          By

          “Numerical simulation of the SOFIA flowfield” Metadata:

          • Title: ➤  Numerical simulation of the SOFIA flowfield
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC - San Jose, CA

          “Numerical simulation of the SOFIA flowfield” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1994
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

          Online Borrowing:

            Online Marketplaces

            Find Numerical simulation of the SOFIA flowfield at online marketplaces:


            6Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode

            By

            “Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode” Metadata:

            • Title: ➤  Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode
            • Author:
            • Language: English
            • Number of Pages: Median: 51
            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center
            • Publish Date:
            • Publish Location: ➤  Hampton, Va - [Washington, D.C.]

            “Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1991
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

            Online Borrowing:

              Online Marketplaces

              Find Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode at online marketplaces:


              7Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual

              By

              “Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual” Metadata:

              • Title: ➤  Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual
              • Author:
              • Language: English
              • Number of Pages: Median: 61
              • Publisher: ➤  National Technical Information Service, distributor - Langley Research Center - National Aeronautics and Space Administration, Langley Research Center
              • Publish Date:
              • Publish Location: [Springfield, Va - Hampton, Va

              “Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1994
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

              Online Borrowing:

                Online Marketplaces

                Find Langley 14- by 22-foot subsonic tunnel test engineer's data acquisition and reduction manual at online marketplaces:


                8Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft

                By

                “Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft” Metadata:

                • Title: ➤  Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft
                • Author:
                • Language: English
                • Number of Pages: Median: 62
                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - Langley Research Center
                • Publish Date:
                • Publish Location: [Springfield, Va - Hampton, Va

                “Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1994
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                Online Borrowing:

                  Online Marketplaces

                  Find Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft at online marketplaces:


                  92-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall

                  By

                  “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:

                  • Title: ➤  2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 559
                  • Publisher: ➤  National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
                  • Publish Date:
                  • Publish Location: ➤  Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va

                  “2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1994
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                  Online Borrowing:

                    Online Marketplaces

                    Find 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall at online marketplaces:


                    10Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing

                    By

                    “Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing” Metadata:

                    • Title: ➤  Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 89
                    • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
                    • Publish Date:
                    • Publish Location: ➤  [Springfield, Va - [Washington, DC] - Hampton, Va

                    “Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1990
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                    Online Borrowing:

                      Online Marketplaces

                      Find Close-range photogrammetric measurement of static deflections for an aeroelastic supercritical wing at online marketplaces:


                      11Wind-tunnel investigation of a full-scale canard-configured general aviation airplane

                      By

                      “Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Metadata:

                      • Title: ➤  Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
                      • Author:
                      • Language: English
                      • Publisher: ➤  National; Aeronautics and Space Administration Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                      • Publish Date:
                      • Publish Location: [s.l.] - [Washington, D.C.]

                      “Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1985
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                      Online Borrowing:

                        Online Marketplaces

                        Find Wind-tunnel investigation of a full-scale canard-configured general aviation airplane at online marketplaces:


                        12Low-speed wind-tunnel tests of single- and counter-rotation propellers

                        By

                        “Low-speed wind-tunnel tests of single- and counter-rotation propellers” Metadata:

                        • Title: ➤  Low-speed wind-tunnel tests of single- and counter-rotation propellers
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 43
                        • Publisher: ➤  National Aeronautics and Space Administration Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                        • Publish Date:
                        • Publish Location: ➤  Hampton, Va - [Springfield, Va - [s.l.] - [Washington, D.C.]

                        “Low-speed wind-tunnel tests of single- and counter-rotation propellers” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1986
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                        Online Borrowing:

                          Online Marketplaces

                          Find Low-speed wind-tunnel tests of single- and counter-rotation propellers at online marketplaces:


                          13Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails

                          By

                          “Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Metadata:

                          • Title: ➤  Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
                          • Publish Date:
                          • Publish Location: [Springfield, Va - Hampton, Va

                          “Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1997
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Access

                          Downloads Are Not Available:

                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                          Online Borrowing:

                            Online Marketplaces

                            Find Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails at online marketplaces:


                            14Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

                            By

                            “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:

                            • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
                            • Author:
                            • Language: English
                            • Number of Pages: Median: 145
                            • Publisher: ➤  National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  Hampton, Va - [Washington, DC - Springfield, Va

                            “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1995
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

                            Online Access

                            Downloads Are Not Available:

                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                            Online Borrowing:

                              Online Marketplaces

                              Find Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊ at online marketplaces:


                              15Control of low-speed turbulent separated flow over a backward-facing ramp

                              By

                              “Control of low-speed turbulent separated flow over a backward-facing ramp” Metadata:

                              • Title: ➤  Control of low-speed turbulent separated flow over a backward-facing ramp
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  Springfield, Va - [Washington, DC

                              “Control of low-speed turbulent separated flow over a backward-facing ramp” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1994
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

                              Online Access

                              Downloads Are Not Available:

                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                              Online Borrowing:

                                Online Marketplaces

                                Find Control of low-speed turbulent separated flow over a backward-facing ramp at online marketplaces:


                                16A laser-based ice shape profilometer for use in icing wind tunnels

                                By

                                “A laser-based ice shape profilometer for use in icing wind tunnels” Metadata:

                                • Title: ➤  A laser-based ice shape profilometer for use in icing wind tunnels
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                “A laser-based ice shape profilometer for use in icing wind tunnels” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1995
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

                                Online Access

                                Downloads Are Not Available:

                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                Online Borrowing:

                                  Online Marketplaces

                                  Find A laser-based ice shape profilometer for use in icing wind tunnels at online marketplaces:


                                  17Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness

                                  By

                                  “Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Metadata:

                                  • Title: ➤  Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
                                  • Publish Date:
                                  • Publish Location: ➤  Springfield, VA - Edwards, Calif

                                  “Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 2001
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

                                  Online Access

                                  Downloads Are Not Available:

                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                  Online Borrowing:

                                    Online Marketplaces

                                    Find Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness at online marketplaces:


                                    18A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process

                                    By

                                    “A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process” Metadata:

                                    • Title: ➤  A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                    • Publish Date:
                                    • Publish Location: Hampton, Va - [Springfield, Va

                                    “A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1998
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

                                    Online Access

                                    Downloads Are Not Available:

                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                    Online Borrowing:

                                      Online Marketplaces

                                      Find A Microsoft project-based planning, tracking, and management tool for the National Transonic Facility's model changeover process at online marketplaces:


                                      19Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack

                                      By

                                      “Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Metadata:

                                      • Title: ➤  Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Dryden Flight Research Center
                                      • Publish Date:
                                      • Publish Location: Edwards, Calif - Hanover, MD

                                      “Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 2001
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
                                      • Access Status: No_ebook

                                      Online Access

                                      Downloads Are Not Available:

                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                      Online Borrowing:

                                        Online Marketplaces

                                        Find Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack at online marketplaces:


                                        20F-18 High Alpha Research Vehicle surface pressures

                                        By

                                        “F-18 High Alpha Research Vehicle surface pressures” Metadata:

                                        • Title: ➤  F-18 High Alpha Research Vehicle surface pressures
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 36
                                        • Publisher: ➤  National Technical Information Service, distributor] - NASA Ames Resarch Center, Dryden Flight Research Facility
                                        • Publish Date:
                                        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                                        “F-18 High Alpha Research Vehicle surface pressures” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1990
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

                                        Online Access

                                        Downloads Are Not Available:

                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                        Online Borrowing:

                                          Online Marketplaces

                                          Find F-18 High Alpha Research Vehicle surface pressures at online marketplaces:


                                          21Hot-bench simulation of the active flexible wing wind-tunnel model

                                          By

                                          “Hot-bench simulation of the active flexible wing wind-tunnel model” Metadata:

                                          • Title: ➤  Hot-bench simulation of the active flexible wing wind-tunnel model
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                          • Publish Date:
                                          • Publish Location: Hampton, Va

                                          “Hot-bench simulation of the active flexible wing wind-tunnel model” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1990
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

                                          Online Access

                                          Downloads Are Not Available:

                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                          Online Borrowing:

                                            Online Marketplaces

                                            Find Hot-bench simulation of the active flexible wing wind-tunnel model at online marketplaces:


                                            22User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel

                                            By

                                            “User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:

                                            • Title: ➤  User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                            • Publish Date:
                                            • Publish Location: ➤  [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va

                                            “User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1992
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

                                            Online Access

                                            Downloads Are Not Available:

                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                            Online Borrowing:

                                              Online Marketplaces

                                              Find User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel at online marketplaces:


                                              23Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept

                                              By

                                              “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Metadata:

                                              • Title: ➤  Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
                                              • Author:
                                              • Language: English
                                              • Number of Pages: Median: 36
                                              • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
                                              • Publish Date:
                                              • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

                                              “Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept” Subjects and Themes:

                                              Edition Identifiers:

                                              Access and General Info:

                                              • First Year Published: 1989
                                              • Is Full Text Available: No
                                              • Is The Book Public: No
                                              • Access Status: No_ebook

                                              Online Access

                                              Downloads Are Not Available:

                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                              Online Borrowing:

                                                Online Marketplaces

                                                Find Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept at online marketplaces:


                                                24Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊

                                                By

                                                “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Metadata:

                                                • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
                                                • Author:
                                                • Language: English
                                                • Number of Pages: Median: 140
                                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
                                                • Publish Date:
                                                • Publish Location: ➤  Springfield, VA - Hampton, Va - [Springfield, VA

                                                “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1995
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

                                                Online Marketplaces

                                                Find Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊ at online marketplaces:


                                                25Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests

                                                By

                                                “Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests” Metadata:

                                                • Title: ➤  Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                “Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1995
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

                                                Online Access

                                                Downloads Are Not Available:

                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                Online Borrowing:

                                                  Online Marketplaces

                                                  Find Fabry-Perot interferometer measurement of static temperature and velocity for ASTOVL model tests at online marketplaces:


                                                  26Low-speed wind tunnel tests of two waverider configuration models

                                                  By

                                                  “Low-speed wind tunnel tests of two waverider configuration models” Metadata:

                                                  • Title: ➤  Low-speed wind tunnel tests of two waverider configuration models
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
                                                  • Publish Date:
                                                  • Publish Location: ➤  Washington, D.C - Springfield, Va

                                                  “Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1995
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

                                                  Online Access

                                                  Downloads Are Not Available:

                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                  Online Borrowing:

                                                    Online Marketplaces

                                                    Find Low-speed wind tunnel tests of two waverider configuration models at online marketplaces:


                                                    27Distributed-roughness effects on stability and transition in swept-wing boundary layers

                                                    By

                                                    “Distributed-roughness effects on stability and transition in swept-wing boundary layers” Metadata:

                                                    • Title: ➤  Distributed-roughness effects on stability and transition in swept-wing boundary layers
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                    • Publish Date:
                                                    • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                    “Distributed-roughness effects on stability and transition in swept-wing boundary layers” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1997
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

                                                    Online Access

                                                    Downloads Are Not Available:

                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                    Online Borrowing:

                                                      Online Marketplaces

                                                      Find Distributed-roughness effects on stability and transition in swept-wing boundary layers at online marketplaces:


                                                      28Key topics for high-lift research

                                                      By

                                                      “Key topics for high-lift research” Metadata:

                                                      • Title: ➤  Key topics for high-lift research
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                      • Publish Date:
                                                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                      “Key topics for high-lift research” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 1996
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

                                                      Online Access

                                                      Downloads Are Not Available:

                                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                      Online Borrowing:

                                                        Online Marketplaces

                                                        Find Key topics for high-lift research at online marketplaces:


                                                        29Navier-Stokes simulation of several high-lift reference H configurations

                                                        By

                                                        “Navier-Stokes simulation of several high-lift reference H configurations” Metadata:

                                                        • Title: ➤  Navier-Stokes simulation of several high-lift reference H configurations
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor - Available from NASA Center for AeroSpace Information
                                                        • Publish Date:
                                                        • Publish Location: ➤  Springfield, VA - Hampton, Va - Hanover, MD

                                                        “Navier-Stokes simulation of several high-lift reference H configurations” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1999
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
                                                        • Access Status: No_ebook

                                                        Online Access

                                                        Downloads Are Not Available:

                                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                        Online Borrowing:

                                                          Online Marketplaces

                                                          Find Navier-Stokes simulation of several high-lift reference H configurations at online marketplaces:


                                                          30The lift-fan aircraft

                                                          By

                                                          “The lift-fan aircraft” Metadata:

                                                          • Title: The lift-fan aircraft
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                                                          • Publish Date:
                                                          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                                          “The lift-fan aircraft” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1995
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
                                                          • Access Status: No_ebook

                                                          Online Access

                                                          Downloads Are Not Available:

                                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                          Online Borrowing:

                                                            Online Marketplaces

                                                            Find The lift-fan aircraft at online marketplaces:


                                                            31Supersonic quiet-tunnel development for laminar-turbulent transition research

                                                            By

                                                            “Supersonic quiet-tunnel development for laminar-turbulent transition research” Metadata:

                                                            • Title: ➤  Supersonic quiet-tunnel development for laminar-turbulent transition research
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                            • Publish Date:
                                                            • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                            “Supersonic quiet-tunnel development for laminar-turbulent transition research” Subjects and Themes:

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1995
                                                            • Is Full Text Available: No
                                                            • Is The Book Public: No
                                                            • Access Status: No_ebook

                                                            Online Access

                                                            Downloads Are Not Available:

                                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                            Online Borrowing:

                                                              Online Marketplaces

                                                              Find Supersonic quiet-tunnel development for laminar-turbulent transition research at online marketplaces:


                                                              32Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel

                                                              By

                                                              “Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Metadata:

                                                              • Title: ➤  Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel
                                                              • Author:
                                                              • Number of Pages: Median: 137
                                                              • Publisher: Langley Research Center
                                                              • Publish Date:
                                                              • Publish Location: Hampton, Va

                                                              “Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel” Subjects and Themes:

                                                              Edition Identifiers:

                                                              Access and General Info:

                                                              • First Year Published: 1981
                                                              • Is Full Text Available: No
                                                              • Is The Book Public: No
                                                              • Access Status: No_ebook

                                                              Online Marketplaces

                                                              Find Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-foot transonic pressure tunnel at online marketplaces:


                                                              33Shock-tunnel combustor testing for hypersonic vehicles

                                                              By

                                                              “Shock-tunnel combustor testing for hypersonic vehicles” Metadata:

                                                              • Title: ➤  Shock-tunnel combustor testing for hypersonic vehicles
                                                              • Author:
                                                              • Language: English
                                                              • Publisher: ➤  MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                              • Publish Date:
                                                              • Publish Location: ➤  Springfield, Va - San Jose, Calif - [Washington, DC

                                                              “Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:

                                                              Edition Identifiers:

                                                              Access and General Info:

                                                              • First Year Published: 1994
                                                              • Is Full Text Available: No
                                                              • Is The Book Public: No
                                                              • Access Status: No_ebook

                                                              Online Access

                                                              Downloads Are Not Available:

                                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                              Online Borrowing:

                                                                Online Marketplaces

                                                                Find Shock-tunnel combustor testing for hypersonic vehicles at online marketplaces:


                                                                34Control of unsteady separated flow associated with the dynamic stall of airfoils

                                                                By

                                                                “Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:

                                                                • Title: ➤  Control of unsteady separated flow associated with the dynamic stall of airfoils
                                                                • Author:
                                                                • Language: English
                                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
                                                                • Publish Date:
                                                                • Publish Location: ➤  Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA

                                                                “Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:

                                                                Edition Identifiers:

                                                                Access and General Info:

                                                                • First Year Published: 1992
                                                                • Is Full Text Available: No
                                                                • Is The Book Public: No
                                                                • Access Status: No_ebook

                                                                Online Access

                                                                Downloads Are Not Available:

                                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                Online Borrowing:

                                                                  Online Marketplaces

                                                                  Find Control of unsteady separated flow associated with the dynamic stall of airfoils at online marketplaces:


                                                                  35Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter

                                                                  By

                                                                  “Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Metadata:

                                                                  • Title: ➤  Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
                                                                  • Publish Date:
                                                                  • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

                                                                  “Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter” Subjects and Themes:

                                                                  Edition Identifiers:

                                                                  Access and General Info:

                                                                  • First Year Published: 1985
                                                                  • Is Full Text Available: No
                                                                  • Is The Book Public: No
                                                                  • Access Status: No_ebook

                                                                  Online Access

                                                                  Downloads Are Not Available:

                                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                  Online Borrowing:

                                                                    Online Marketplaces

                                                                    Find Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter at online marketplaces:


                                                                    36Performance study for inlet installations

                                                                    By

                                                                    “Performance study for inlet installations” Metadata:

                                                                    • Title: ➤  Performance study for inlet installations
                                                                    • Author:
                                                                    • Language: English
                                                                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                                    • Publish Date:
                                                                    • Publish Location: [Springfield, Va - Hampton, Va

                                                                    “Performance study for inlet installations” Subjects and Themes:

                                                                    Edition Identifiers:

                                                                    Access and General Info:

                                                                    • First Year Published: 1992
                                                                    • Is Full Text Available: No
                                                                    • Is The Book Public: No
                                                                    • Access Status: No_ebook

                                                                    Online Access

                                                                    Downloads Are Not Available:

                                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                    Online Borrowing:

                                                                      Online Marketplaces

                                                                      Find Performance study for inlet installations at online marketplaces:


                                                                      37Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

                                                                      By

                                                                      “Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Metadata:

                                                                      • Title: ➤  Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle
                                                                      • Author:
                                                                      • Language: English
                                                                      • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                                      • Publish Date:
                                                                      • Publish Location: ➤  [Washington, D.C.] - Springfield, Va

                                                                      “Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle” Subjects and Themes:

                                                                      Edition Identifiers:

                                                                      Access and General Info:

                                                                      • First Year Published: 1985
                                                                      • Is Full Text Available: No
                                                                      • Is The Book Public: No
                                                                      • Access Status: No_ebook

                                                                      Online Access

                                                                      Downloads Are Not Available:

                                                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                      Online Borrowing:

                                                                        Online Marketplaces

                                                                        Find Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle at online marketplaces:


                                                                        38Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate

                                                                        By

                                                                        “Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Metadata:

                                                                        • Title: ➤  Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
                                                                        • Author:
                                                                        • Language: English
                                                                        • Number of Pages: Median: 18
                                                                        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service - Langley Research Center
                                                                        • Publish Date:
                                                                        • Publish Location: ➤  Hampton, Va - Washington, D.C - Springfield, Va

                                                                        “Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Subjects and Themes:

                                                                        Edition Identifiers:

                                                                        Access and General Info:

                                                                        • First Year Published: 1986
                                                                        • Is Full Text Available: No
                                                                        • Is The Book Public: No
                                                                        • Access Status: No_ebook

                                                                        Online Access

                                                                        Downloads Are Not Available:

                                                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                        Online Borrowing:

                                                                          Online Marketplaces

                                                                          Find Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate at online marketplaces:


                                                                          39Ultra-high bypass ratio jet noise

                                                                          By

                                                                          “Ultra-high bypass ratio jet noise” Metadata:

                                                                          • Title: ➤  Ultra-high bypass ratio jet noise
                                                                          • Author:
                                                                          • Language: English
                                                                          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                          “Ultra-high bypass ratio jet noise” Subjects and Themes:

                                                                          Edition Identifiers:

                                                                          Access and General Info:

                                                                          • First Year Published: 1994
                                                                          • Is Full Text Available: No
                                                                          • Is The Book Public: No
                                                                          • Access Status: No_ebook

                                                                          Online Access

                                                                          Downloads Are Not Available:

                                                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                          Online Borrowing:

                                                                            Online Marketplaces

                                                                            Find Ultra-high bypass ratio jet noise at online marketplaces:


                                                                            40Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

                                                                            By

                                                                            “Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Metadata:

                                                                            • Title: ➤  Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions
                                                                            • Author:
                                                                            • Language: English
                                                                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                            • Publish Date:
                                                                            • Publish Location: ➤  Springfield, Va - [Washington, DC - [Washington, D.C

                                                                            “Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions” Subjects and Themes:

                                                                            Edition Identifiers:

                                                                            Access and General Info:

                                                                            • First Year Published: 1994
                                                                            • Is Full Text Available: No
                                                                            • Is The Book Public: No
                                                                            • Access Status: No_ebook

                                                                            Online Access

                                                                            Downloads Are Not Available:

                                                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                            Online Borrowing:

                                                                              Online Marketplaces

                                                                              Find Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions at online marketplaces:


                                                                              41Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation

                                                                              By

                                                                              “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:

                                                                              • Title: ➤  Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
                                                                              • Author:
                                                                              • Language: English
                                                                              • Publisher: ➤  North Carolina State University, Dept. of Mechanical and Aerospace Engineering
                                                                              • Publish Date:
                                                                              • Publish Location: Raleigh, [N.C.]

                                                                              “Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:

                                                                              Edition Identifiers:

                                                                              Access and General Info:

                                                                              • First Year Published: 1990
                                                                              • Is Full Text Available: No
                                                                              • Is The Book Public: No
                                                                              • Access Status: No_ebook

                                                                              Online Access

                                                                              Downloads Are Not Available:

                                                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                              Online Borrowing:

                                                                                Online Marketplaces

                                                                                Find Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation at online marketplaces:


                                                                                42Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data

                                                                                By

                                                                                “Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Metadata:

                                                                                • Title: ➤  Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
                                                                                • Author:
                                                                                • Language: English
                                                                                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Dept. of Mechanical and Aeronautical Engineering, University of California
                                                                                • Publish Date:
                                                                                • Publish Location: ➤  [Washington, DC - Springfield, Va - Davis, CA

                                                                                “Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data” Subjects and Themes:

                                                                                Edition Identifiers:

                                                                                Access and General Info:

                                                                                • First Year Published: 1995
                                                                                • Is Full Text Available: No
                                                                                • Is The Book Public: No
                                                                                • Access Status: No_ebook

                                                                                Online Access

                                                                                Downloads Are Not Available:

                                                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                Online Borrowing:

                                                                                  Online Marketplaces

                                                                                  Find Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data at online marketplaces:


                                                                                  43Non-linear boundary-layer receptivity due to distributed surface roughness

                                                                                  By

                                                                                  “Non-linear boundary-layer receptivity due to distributed surface roughness” Metadata:

                                                                                  • Title: ➤  Non-linear boundary-layer receptivity due to distributed surface roughness
                                                                                  • Author:
                                                                                  • Language: English
                                                                                  • Publisher: ➤  National Aeronautics and Space Administration - Old Dominion University Research Foundation, Dept. of Mechanical Engineering, College of Engineering & Technology - National Technical Information Service, distributor
                                                                                  • Publish Date:
                                                                                  • Publish Location: ➤  [Washington, D.C - Norfolk, Va - Springfield, Va

                                                                                  “Non-linear boundary-layer receptivity due to distributed surface roughness” Subjects and Themes:

                                                                                  Edition Identifiers:

                                                                                  Access and General Info:

                                                                                  • First Year Published: 1995
                                                                                  • Is Full Text Available: No
                                                                                  • Is The Book Public: No
                                                                                  • Access Status: No_ebook

                                                                                  Online Access

                                                                                  Downloads Are Not Available:

                                                                                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                  Online Borrowing:

                                                                                    Online Marketplaces

                                                                                    Find Non-linear boundary-layer receptivity due to distributed surface roughness at online marketplaces:


                                                                                    44Supersonic laminar flow control research

                                                                                    By

                                                                                    “Supersonic laminar flow control research” Metadata:

                                                                                    • Title: ➤  Supersonic laminar flow control research
                                                                                    • Author:
                                                                                    • Language: English
                                                                                    • Publisher: ➤  Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
                                                                                    • Publish Date:
                                                                                    • Publish Location: ➤  Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va

                                                                                    “Supersonic laminar flow control research” Subjects and Themes:

                                                                                    Edition Identifiers:

                                                                                    Access and General Info:

                                                                                    • First Year Published: 1995
                                                                                    • Is Full Text Available: No
                                                                                    • Is The Book Public: No
                                                                                    • Access Status: No_ebook

                                                                                    Online Access

                                                                                    Downloads Are Not Available:

                                                                                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                    Online Borrowing:

                                                                                      Online Marketplaces

                                                                                      Find Supersonic laminar flow control research at online marketplaces:


                                                                                      45Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel

                                                                                      By

                                                                                      “Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel” Metadata:

                                                                                      • Title: ➤  Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel
                                                                                      • Author:
                                                                                      • Language: English
                                                                                      • Number of Pages: Median: 21
                                                                                      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch - For sale by the National Technical Information Service] - NASA
                                                                                      • Publish Date:
                                                                                      • Publish Location: ➤  [Washington, D.C.] - Washington - [Springfield, Va

                                                                                      “Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel” Subjects and Themes:

                                                                                      Edition Identifiers:

                                                                                      Access and General Info:

                                                                                      • First Year Published: 1986
                                                                                      • Is Full Text Available: No
                                                                                      • Is The Book Public: No
                                                                                      • Access Status: No_ebook

                                                                                      Online Access

                                                                                      Downloads Are Not Available:

                                                                                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                      Online Borrowing:

                                                                                        Online Marketplaces

                                                                                        Find Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel at online marketplaces:


                                                                                        46Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

                                                                                        By

                                                                                        “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:

                                                                                        • Title: ➤  Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
                                                                                        • Author:
                                                                                        • Language: English
                                                                                        • Number of Pages: Median: 48
                                                                                        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
                                                                                        • Publish Date:
                                                                                        • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

                                                                                        “Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Subjects and Themes:

                                                                                        Edition Identifiers:

                                                                                        Access and General Info:

                                                                                        • First Year Published: 1991
                                                                                        • Is Full Text Available: No
                                                                                        • Is The Book Public: No
                                                                                        • Access Status: No_ebook

                                                                                        Online Access

                                                                                        Downloads Are Not Available:

                                                                                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                        Online Borrowing:

                                                                                          Online Marketplaces

                                                                                          Find Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil at online marketplaces:


                                                                                          47A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel

                                                                                          By

                                                                                          “A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Metadata:

                                                                                          • Title: ➤  A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel
                                                                                          • Author:
                                                                                          • Language: English
                                                                                          • Number of Pages: Median: 56
                                                                                          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
                                                                                          • Publish Date:
                                                                                          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                                                                          “A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel” Subjects and Themes:

                                                                                          Edition Identifiers:

                                                                                          Access and General Info:

                                                                                          • First Year Published: 1989
                                                                                          • Is Full Text Available: No
                                                                                          • Is The Book Public: No
                                                                                          • Access Status: No_ebook

                                                                                          Online Access

                                                                                          Downloads Are Not Available:

                                                                                          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                          Online Borrowing:

                                                                                            Online Marketplaces

                                                                                            Find A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel at online marketplaces:


                                                                                            48Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4

                                                                                            By

                                                                                            “Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Metadata:

                                                                                            • Title: ➤  Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4
                                                                                            • Author:
                                                                                            • Language: English
                                                                                            • Number of Pages: Median: 31
                                                                                            • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
                                                                                            • Publish Date:
                                                                                            • Publish Location: ➤  Edwards, Calif - Springfield, VA

                                                                                            “Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4” Subjects and Themes:

                                                                                            Edition Identifiers:

                                                                                            Access and General Info:

                                                                                            • First Year Published: 1990
                                                                                            • Is Full Text Available: No
                                                                                            • Is The Book Public: No
                                                                                            • Access Status: No_ebook

                                                                                            Online Access

                                                                                            Downloads Are Not Available:

                                                                                            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                            Online Borrowing:

                                                                                              Online Marketplaces

                                                                                              Find Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 at online marketplaces:


                                                                                              49Measurements of unsteady pressure and structural response for an elastic supercritical wing

                                                                                              By

                                                                                              “Measurements of unsteady pressure and structural response for an elastic supercritical wing” Metadata:

                                                                                              • Title: ➤  Measurements of unsteady pressure and structural response for an elastic supercritical wing
                                                                                              • Author:
                                                                                              • Language: English
                                                                                              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
                                                                                              • Publish Date:
                                                                                              • Publish Location: ➤  Hampton - Hampton, Va - [Springfield, Va

                                                                                              “Measurements of unsteady pressure and structural response for an elastic supercritical wing” Subjects and Themes:

                                                                                              Edition Identifiers:

                                                                                              Access and General Info:

                                                                                              • First Year Published: 1994
                                                                                              • Is Full Text Available: No
                                                                                              • Is The Book Public: No
                                                                                              • Access Status: No_ebook

                                                                                              Online Access

                                                                                              Downloads Are Not Available:

                                                                                              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                              Online Borrowing:

                                                                                                Online Marketplaces

                                                                                                Find Measurements of unsteady pressure and structural response for an elastic supercritical wing at online marketplaces:


                                                                                                50Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers

                                                                                                By

                                                                                                “Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” Metadata:

                                                                                                • Title: ➤  Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers
                                                                                                • Author:
                                                                                                • Language: English
                                                                                                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                                                • Publish Date:
                                                                                                • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                                                                “Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers” Subjects and Themes:

                                                                                                Edition Identifiers:

                                                                                                Access and General Info:

                                                                                                • First Year Published: 1985
                                                                                                • Is Full Text Available: No
                                                                                                • Is The Book Public: No
                                                                                                • Access Status: No_ebook

                                                                                                Online Access

                                                                                                Downloads Are Not Available:

                                                                                                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

                                                                                                Online Borrowing:

                                                                                                  Online Marketplaces

                                                                                                  Find Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers at online marketplaces:



                                                                                                  Wiki

                                                                                                  Source: Wikipedia

                                                                                                  Wikipedia Results

                                                                                                  Search Results from Wikipedia

                                                                                                  Wind tunnel

                                                                                                  is conducted in the test section of the wind tunnel and a complete tunnel configuration includes air ducting to and from the test section and a device

                                                                                                  Supersonic wind tunnel

                                                                                                  A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2<M<5) The Mach number and flow are determined by the nozzle geometry. The

                                                                                                  Lockheed Martin X-59 Quesst

                                                                                                  vision system (XVS) was flight tested on a King Air at NASA Langley. This is to be followed by high speed wind tunnel tests to verify inlet performance predictions

                                                                                                  AGARD-B wind tunnel model

                                                                                                  standards of comparison between wind tunnels and improve the validity of wind tunnel tests. Among the standard wind tunnel models, AGARD model configuration

                                                                                                  Hypersonic Technology Demonstrator Vehicle

                                                                                                  setting up a much-needed hypersonic wind tunnel at Hyderabad's Missile Complex. The advanced Hypersonic Wind Tunnel (HWT) test facility was finally commissioned

                                                                                                  CAC CA-23

                                                                                                  made at different scales, with hundreds of detailed drawings, plus wind tunnel tests proving the delta wing was more than satisfactory. The program was

                                                                                                  Nissan GT-R

                                                                                                  model served as a comparable datum against the GT-R model. Initial wind tunnel tests with the GT-R model yielded a drag coefficient of Cd=0.32. As the

                                                                                                  Project FIRE

                                                                                                  spacecraft materials. Project FIRE used both ground testing in wind tunnels and flight tests to test the effects of reentry heating on spacecraft materials

                                                                                                  Tsing Ma Bridge

                                                                                                  in Scotland and the Severn Bridge in England. The objectives of the wind tunnel studies were to demonstrate the safety of the structure under construction

                                                                                                  Wright brothers

                                                                                                  Lilienthal's published data were fairly accurate for the tests he had done. Before the detailed wind tunnel tests, Wilbur traveled to Chicago at Chanute's invitation