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1Study of optical techniques for the Ames unitary wind tunnels

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“Study of optical techniques for the Ames unitary wind tunnels” Metadata:

  • Title: ➤  Study of optical techniques for the Ames unitary wind tunnels
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Springfield, Va.? - Springfield, Va - San Jose, CA - [Washington, D.C

“Study of optical techniques for the Ames unitary wind tunnels” 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

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    2Recommended Practice

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    Book's cover

    “Recommended Practice” Metadata:

    • Title: Recommended Practice
    • Author: ➤  
    • Language: English
    • Number of Pages: Median: 74
    • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast
    • Publish Date:

    “Recommended Practice” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 2002
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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      3Hot-jet simulation in cryogenic wind tunnels

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      “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.

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        4Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

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        “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:

        • Title: ➤  Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
        • Author:
        • Language: English
        • Number of Pages: Median: 211
        • 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 investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1983
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        5Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊

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        “Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Metadata:

        • Title: ➤  Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
        • Author:
        • Language: English
        • Number of Pages: Median: 149
        • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Washington, DC - Springfield, Va - Washington

        “Wind-tunnel pressure data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1977
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        6Langley 8-ft. HTT test 139 gas analyses

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        “Langley 8-ft. HTT test 139 gas analyses” Metadata:

        • Title: ➤  Langley 8-ft. HTT test 139 gas analyses
        • Author:
        • Language: English
        • Number of Pages: Median: 192
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va - [Springfield, Va

        “Langley 8-ft. HTT test 139 gas analyses” 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.

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          7KC-135 Winglet Program Review

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          “KC-135 Winglet Program Review” Metadata:

          • Title: KC-135 Winglet Program Review
          • Author: ➤  
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
          • Publish Date:
          • Publish Location: [Washington, D.C.?]

          “KC-135 Winglet Program Review” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1982
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

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            8Wind Tunnel Testing of High-Rise Buildings

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            “Wind Tunnel Testing of High-Rise Buildings” Metadata:

            • Title: ➤  Wind Tunnel Testing of High-Rise Buildings
            • Author:
            • Language: English
            • Publisher: ➤  Routledge - Taylor & Francis Group - CRC Press LLC
            • Publish Date:

            “Wind Tunnel Testing of High-Rise Buildings” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 2013
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            9Wind-tunnel testing

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            “Wind-tunnel testing” Metadata:

            • Title: Wind-tunnel testing
            • Author:
            • Language: English
            • Number of Pages: Median: 511
            • Publisher: ➤  Chapman and Hall - Wiley - WILEY, JOHN @ & SONS
            • Publish Date:
            • Publish Location: New York - London

            “Wind-tunnel testing” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1947
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            10Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊

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            “Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Metadata:

            • Title: ➤  Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊
            • Author:
            • Language: English
            • Number of Pages: Median: 149
            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - Washington, D.C

            “Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1979
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            Find Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from -4 ̊to 60 ̊ at online marketplaces:


            11Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results

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            “Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results” Metadata:

            • Title: ➤  Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results
            • Author:
            • Language: English
            • Number of Pages: Median: 52
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
            • Publish Date:
            • Publish Location: ➤  Washington, D.C - [Springfield, Va

            “Evaluation of wind-tunnel gust response technique correlations with analytical and flight test results” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1979
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            12Wind-tunnel testing

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            “Wind-tunnel testing” Metadata:

            • Title: Wind-tunnel testing
            • Author:
            • Language: English
            • Number of Pages: Median: 511
            • Publisher: J. Wiley - Wiley
            • Publish Date:
            • Publish Location: New York

            “Wind-tunnel testing” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1947
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            13The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel

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            “The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel” Metadata:

            • Title: ➤  The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel
            • Author:
            • Language: English
            • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
            • Publish Date:
            • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

            “The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot 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.

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              14Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

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              “Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Metadata:

              • Title: ➤  Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: Hampton, Va - [Springfield, Va

              “Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” 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.

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                15Wind-tunnel test of an articulated helicopter rotor model with several tip shapes

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                “Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” Metadata:

                • Title: ➤  Wind-tunnel test of an articulated helicopter rotor model with several tip shapes
                • Author:
                • Language: English
                • Number of Pages: Median: 92
                • Publisher: ➤  Fo r sale by the National Technical Information Service] - National Aeronautics and Space Administrat ion, Scientific and Technical Information Branch
                • Publish Date:
                • Publish Location: ➤  [Springfield, Va - Washington, D.C

                “Wind-tunnel test of an articulated helicopter rotor model with several tip shapes” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

                • First Year Published: 1980
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

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                16Aeronautical facilities catalogue

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                “Aeronautical facilities catalogue” Metadata:

                • Title: ➤  Aeronautical facilities catalogue
                • Author:
                • Language: English
                • Publisher: ➤  Scientific and Technical Information Branch, National Aeronautics and Space Administration - For sale by the National Technical Information Service] - For sale by the National Aeronautics and Space Administration] - For sale by the Supt. of Docs., U.S. G.P.O.]
                • Publish Date:
                • Publish Location: ➤  Washington, DC - [Springfield, Va

                “Aeronautical facilities catalogue” 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.

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                  17Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

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                  “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Metadata:

                  • Title: ➤  Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 193
                  • 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

                  “Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1983
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

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                  18Finite-rate water condensation in combustion-heated wind tunnels

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                  “Finite-rate water condensation in combustion-heated wind tunnels” Metadata:

                  • Title: ➤  Finite-rate water condensation in combustion-heated wind tunnels
                  • Author:
                  • Language: English
                  • Number of Pages: Median: 69
                  • 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: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

                  “Finite-rate water condensation in combustion-heated wind tunnels” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1988
                  • 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.

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                    19Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)

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                    “Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)” Metadata:

                    • Title: ➤  Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 39
                    • Publisher: ➤  Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
                    • Publish Date:
                    • Publish Location: ➤  [Cleveland, Ohio] - Hanover, MD

                    “Aero-thermal calibration of the NASA Glenn icing research tunnel (2000 tests)” 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.

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                      20Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers

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                      “Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers” Metadata:

                      • Title: ➤  Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Facility - National Technical Information Service, [distributor]
                      • Publish Date:
                      • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                      “Flight and wind-tunnel calibrations of a flush airdata sensor at high angles of attack and sideslip and at supersonic mach numbers” 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.

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                        21X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results

                        By

                        “X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results” Metadata:

                        • Title: ➤  X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration,Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

                        “X-29A longitudinal and directional force and moment supplemental transonic wind tunnel test results” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1984
                        • 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.

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                          22On-line analysis capabilities developed to support the AFW wind-tunnel tests

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                          “On-line analysis capabilities developed to support the AFW wind-tunnel tests” Metadata:

                          • Title: ➤  On-line analysis capabilities developed to support the AFW wind-tunnel tests
                          • 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, Va - [Springfield, Va

                          “On-line analysis capabilities developed to support the AFW wind-tunnel tests” 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.

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                            23Validation of vortex-lattice method for loads on wings in lift-generated wakes

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                            “Validation of vortex-lattice method for loads on wings in lift-generated wakes” Metadata:

                            • Title: ➤  Validation of vortex-lattice method for loads on wings in lift-generated wakes
                            • Author:
                            • Language: English
                            • Publisher: ➤  American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  Springfield, Va - Washington, DC

                            “Validation of vortex-lattice method for loads on wings in lift-generated wakes” 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.

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                              24NASA Lewis 9-by 15-foot low-speed wind tunnel user manual

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                              “NASA Lewis 9-by 15-foot low-speed wind tunnel user manual” Metadata:

                              • Title: ➤  NASA Lewis 9-by 15-foot low-speed wind tunnel user manual
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                              “NASA Lewis 9-by 15-foot low-speed wind tunnel user manual” 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.

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                                25A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel

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                                “A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel” Metadata:

                                • Title: ➤  A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel
                                • Author:
                                • Language: English
                                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                                “A three-dimensional orthogonal laser velocimeter for the NASA Ames 7- by 10-foot wind tunnel” 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.

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                                  26The 13-inch magnetic suspension and balance system wind tunnel

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                                  “The 13-inch magnetic suspension and balance system wind tunnel” Metadata:

                                  • Title: ➤  The 13-inch magnetic suspension and balance system wind tunnel
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 45
                                  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Division - Langley Research Center
                                  • Publish Date:
                                  • Publish Location: ➤  [Washington, DC] - Hampton, Va - [Springfield, Va

                                  “The 13-inch magnetic suspension and balance system 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

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                                    27Wind-tunnel investigation of an advanced general aviation canard configuration

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                                    “Wind-tunnel investigation of an advanced general aviation canard configuration” Metadata:

                                    • Title: ➤  Wind-tunnel investigation of an advanced general aviation canard configuration
                                    • Author:
                                    • Language: English
                                    • Number of Pages: Median: 45
                                    • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
                                    • Publish Date:
                                    • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                    “Wind-tunnel investigation of an advanced general aviation canard configuration” Subjects and Themes:

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                                    Access and General Info:

                                    • First Year Published: 1984
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                    28Wind-tunnel technique

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                                    “Wind-tunnel technique” Metadata:

                                    • Title: Wind-tunnel technique
                                    • Author:
                                    • Language: English
                                    • Number of Pages: Median: 702
                                    • Publisher: Pitman
                                    • Publish Date:
                                    • Publish Location: London

                                    “Wind-tunnel technique” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1952
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                    29Guide: Assessing Experimental Uncertainty

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                                    Book's cover

                                    “Guide: Assessing Experimental Uncertainty” Metadata:

                                    • Title: ➤  Guide: Assessing Experimental Uncertainty
                                    • Author: ➤  
                                    • Language: English
                                    • Number of Pages: Median: 83
                                    • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast - AIAA (American Institute of Aeronautics & Astronautics)
                                    • Publish Date:

                                    “Guide: Assessing Experimental Uncertainty” Subjects and Themes:

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                                    Access and General Info:

                                    • First Year Published: 2003
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

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                                      30J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field

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                                      “J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field” Metadata:

                                      • Title: ➤  J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field
                                      • Author:
                                      • Language: English
                                      • Number of Pages: Median: 179
                                      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
                                      • Publish Date:
                                      • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va - [Washington, DC]

                                      “J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field” 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

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                                        31Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel

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                                        “Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” Metadata:

                                        • Title: ➤  Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel
                                        • Author:
                                        • Language: English
                                        • Number of Pages: Median: 45
                                        • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
                                        • Publish Date:
                                        • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va - [Washington, DC]

                                        “Large-scale aeroacoustic research feasibility and conceptual design of test-section inserts for the Ames 80- by 120-foot wind tunnel” 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

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                                          32A description of devices used in the study of wind erosion of soils

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                                          “A description of devices used in the study of wind erosion of soils” Metadata:

                                          • Title: ➤  A description of devices used in the study of wind erosion of soils
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 90
                                          • Publisher: ➤  Oxonian Press - Oxonian - Balkema
                                          • Publish Date:
                                          • Publish Location: Rotterdam - New Delhi

                                          “A description of devices used in the study of wind erosion of soils” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1984
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                          33Low-speed wind tunnel testing

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                                          Book's cover

                                          “Low-speed wind tunnel testing” Metadata:

                                          • Title: Low-speed wind tunnel testing
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 713
                                          • Publisher: ➤  Wiley - Wiley & Sons, Limited, John - WILEY
                                          • Publish Date:
                                          • Publish Location: New York

                                          “Low-speed wind tunnel testing” Subjects and Themes:

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

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                                          34Wind-tunnel experiments on divergence of forward-swept wings

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                                          “Wind-tunnel experiments on divergence of forward-swept wings” Metadata:

                                          • Title: ➤  Wind-tunnel experiments on divergence of forward-swept wings
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 46
                                          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va. : For sale by the National Technical Information Service] - Washington, D.C

                                          “Wind-tunnel experiments on divergence of forward-swept wings” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1980
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                          35Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6

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                                          “Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6” Metadata:

                                          • Title: ➤  Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6
                                          • Author:
                                          • Language: English
                                          • Number of Pages: Median: 23
                                          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va. : For sale by the National Technical Information Service] - Washington, D.C

                                          “Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6” 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

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                                          36The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models

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                                          “The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” Metadata:

                                          • Title: ➤  The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  Flight Research Laboratory, University of Kansas, Center for Research Inc.
                                          • Publish Date:
                                          • Publish Location: Lawrence, Kan

                                          “The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1984
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

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                                            37Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps

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                                            “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Metadata:

                                            • Title: ➤  Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
                                            • Publish Date:
                                            • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                            “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1987
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

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                                              38A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter

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                                              “A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter” Metadata:

                                              • Title: ➤  A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter
                                              • Author:
                                              • Language: English
                                              • Number of Pages: Median: 45
                                              • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
                                              • Publish Date:
                                              • Publish Location: [Washington] - Springfield, Va

                                              “A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter” Subjects and Themes:

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                                              Access and General Info:

                                              • First Year Published: 1978
                                              • Is Full Text Available: No
                                              • Is The Book Public: No
                                              • Access Status: No_ebook

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                                              39Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack

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                                              “Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack” Metadata:

                                              • Title: ➤  Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                              • Publish Date:
                                              • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                              “Low-speed wind tunnel performance of high-speed counterrotation propellers at angle-of-attack” 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

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                                                40In-situ technique for checking the calibration of platinum resistance thermometers

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                                                “In-situ technique for checking the calibration of platinum resistance thermometers” Metadata:

                                                • Title: ➤  In-situ technique for checking the calibration of platinum resistance thermometers
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                                                • Publish Date:
                                                • Publish Location: Hampton, Va - [Springfield, Va

                                                “In-situ technique for checking the calibration of platinum resistance thermometers” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1987
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

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                                                  41User manual for 0.3-M TCT wall-interference assessment/correction procedure

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                                                  “User manual for 0.3-M TCT wall-interference assessment/correction procedure” Metadata:

                                                  • Title: ➤  User manual for 0.3-M TCT wall-interference assessment/correction procedure
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
                                                  • Publish Date:
                                                  • Publish Location: Hampton, Va - [Springfield, Va

                                                  “User manual for 0.3-M TCT wall-interference assessment/correction procedure” 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

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                                                    42Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane

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                                                    “Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane” Metadata:

                                                    • Title: ➤  Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 32
                                                    • 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

                                                    “Flight and wind-tunnel comparisons of the inlet/airframe interaction of the F-15 airplane” Subjects and Themes:

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                                                    Access and General Info:

                                                    • First Year Published: 1984
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                    43Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section

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                                                    “Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section” Metadata:

                                                    • Title: ➤  Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 84
                                                    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                                    • Publish Date:
                                                    • Publish Location: ➤  Washington, D.C - [Springfield, Va

                                                    “Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section” 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

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                                                    44Wind-tunnel study of wind loading on a compliant offshore platform

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                                                    “Wind-tunnel study of wind loading on a compliant offshore platform” Metadata:

                                                    • Title: ➤  Wind-tunnel study of wind loading on a compliant offshore platform
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 28
                                                    • Publisher: ➤  The Standards - Order from National Technical Information Service (NTIS)
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Springfield, VA - Washington, DC

                                                    “Wind-tunnel study of wind loading on a compliant offshore platform” Subjects and Themes:

                                                    Edition Identifiers:

                                                    Access and General Info:

                                                    • First Year Published: 1984
                                                    • Is Full Text Available: No
                                                    • Is The Book Public: No
                                                    • Access Status: No_ebook

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                                                    45Wind-tunnel free-flight investigation of a supersonic persistence fighter

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                                                    “Wind-tunnel free-flight investigation of a supersonic persistence fighter” Metadata:

                                                    • Title: ➤  Wind-tunnel free-flight investigation of a supersonic persistence fighter
                                                    • Author:
                                                    • Language: English
                                                    • Number of Pages: Median: 59
                                                    • 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, DC] - [Springfield, Va - Hampton, Va

                                                    “Wind-tunnel free-flight investigation of a supersonic persistence fighter” 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

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                                                      46Experiments in a three-dimensional adaptive-wall wind tunnel

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                                                      “Experiments in a three-dimensional adaptive-wall wind tunnel” Metadata:

                                                      • Title: ➤  Experiments in a three-dimensional adaptive-wall wind tunnel
                                                      • Author:
                                                      • Language: English
                                                      • Number of Pages: Median: 29
                                                      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                                      • Publish Date:
                                                      • Publish Location: ➤  Washington, D.C - [Springfield, Va

                                                      “Experiments in a three-dimensional adaptive-wall wind tunnel” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 1983
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

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                                                      47Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line

                                                      By

                                                      “Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line” Metadata:

                                                      • Title: ➤  Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                                      • Publish Date:
                                                      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

                                                      “Wind-tunnel investigation of aerodynamic efficiency of three planar ellipyical wings with curvature of quarter-chord line” 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

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                                                        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

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                                                          49Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces

                                                          By

                                                          “Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces” Metadata:

                                                          • Title: ➤  Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces
                                                          • Author:
                                                          • Language: English
                                                          • Number of Pages: Median: 34
                                                          • Publisher: ➤  for sale by the National Technical Information Office - National Aeronautics and Space Administration, Scientific and Technical Information Office
                                                          • Publish Date:
                                                          • Publish Location: Springfield, Va - [Washington]

                                                          “Dynamic wind-tunnel tests of an aeromechanical gust-alleviation system using several different combinations of control surfaces” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1978
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
                                                          • Access Status: No_ebook

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                                                          50Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations

                                                          By

                                                          “Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations” Metadata:

                                                          • Title: ➤  Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Aeronautics and Space Administration
                                                          • Publish Date:
                                                          • Publish Location: [Washington, DC]

                                                          “Summary of low-speed wind tunnel results of several high-speed counterrotation propeller configurations” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1988
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
                                                          • Access Status: No_ebook

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                                                          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.

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                                                            Wind tunnel

                                                            inventor Poul la Cour used wind tunnels to develop wind turbines in the early 1890s. Carl Rickard Nyberg used a wind tunnel to design his Flugan starting

                                                            Vertical wind tunnel

                                                            A vertical wind tunnel (VWT) is a wind tunnel that moves air up in a vertical column. Unlike standard wind tunnels, which have test sections that are

                                                            List of wind tunnels

                                                            This is an alphabetical list of wind tunnels. "A2 wind tunnel". Retrieved 26 January 2024. "ACE Climatic Wind Tunnel". Retrieved 26 January 2024. "Fly

                                                            Hypersonic wind tunnel

                                                            facilities like blow-down wind tunnels are designed and installed to simulate the hypersonic flow. A hypersonic wind tunnel comprises in flow direction

                                                            Supersonic wind tunnel

                                                            supersonic wind tunnel is enormous, of the order of 50 MW per square meter of test section cross-sectional area. For this reason, most wind tunnels operate

                                                            Propulsion Wind Tunnel Facility

                                                            Propulsion Wind Tunnel Facility, located at Arnold Engineering Development Complex, Arnold Air Force Base, Tennessee, holds three wind tunnels: the 16-foot

                                                            Compressible flow

                                                            principle behind the wind tunnel is that a large pressure difference is maintained upstream to downstream, driving the flow. Wind tunnels can be divided into

                                                            European Transonic Wind Tunnel

                                                            transonic wind tunnel (ETW) is a high-Reynolds-number transonic wind tunnel using nitrogen as the test gas. It is one of the world's largest cryogenic wind tunnels

                                                            Trisonic Wind Tunnel

                                                            known trisonic wind tunnel was dated to 1950 and was located in El Segundo, California before it closed in 2007. Other trisonic wind tunnels currently in

                                                            German Aeronautical Research Institute

                                                            Institute of Aerodynamics had five wind tunnels, while the Institute of Gas Dynamics had its own high-speed tunnel; both were at the southern end of the