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1Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code

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“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” Metadata:

  • Title: ➤  Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code
  • Author:
  • Language: English
  • Number of Pages: Median: 77
  • Publisher: ➤  Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - Springfield, VA - [Springfield, Va

“Subsonic analysis of 0.04-scale F-16XL models using an unstructured Euler code” 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

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

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    “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

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      3High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation

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      “High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” Metadata:

      • Title: ➤  High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
      • Author:
      • Language: English
      • Number of Pages: Median: 51
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

      “High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation” 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

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        4F-18 High Alpha Research Vehicle surface pressures

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        “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

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          5Laser scanning system for pressure and temperature paints

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          “Laser scanning system for pressure and temperature paints” Metadata:

          • Title: ➤  Laser scanning system for pressure and temperature paints
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Springfield, Va - [Washington, DC

          “Laser scanning system for pressure and temperature paints” 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:

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            6Rocket-based combined cycle engine technology development

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            “Rocket-based combined cycle engine technology development” Metadata:

            • Title: ➤  Rocket-based combined cycle engine technology development
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion - National Aeronautics and Space Administration, distributor]
            • Publish Date:
            • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

            “Rocket-based combined cycle engine technology development” 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:

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              7Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction

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              “Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction” Metadata:

              • Title: ➤  Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction
              • Author:
              • Language: English
              • Number of Pages: Median: 67
              • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
              • Publish Date:
              • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

              “Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction” 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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                8Measurements of unsteady pressure and structural response for an elastic supercritical wing

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                “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

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                  9Analysis of two-phase flow in damper seals for cryogenic turbomachinery

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                  “Analysis of two-phase flow in damper seals for cryogenic turbomachinery” Metadata:

                  • Title: ➤  Analysis of two-phase flow in damper seals for cryogenic turbomachinery
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Aeronautics and Space Administration - Texas A&M University, Mechanical Engineering Dept. - National Technical Information Service, distributor
                  • Publish Date:
                  • Publish Location: ➤  [Washington, DC - [College Station, Tex.] - Springfield, Va

                  “Analysis of two-phase flow in damper seals for cryogenic turbomachinery” 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:

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                    10Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

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                    “Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Metadata:

                    • Title: ➤  Enhanced design of turbo-jet LPT by separation control using phased plasma actuators
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service [distributor - Available from NASA Center for Aerospace Administration - National Aeronautics and Space Administration, Glenn Research Center
                    • Publish Date:
                    • Publish Location: ➤  Springfield, VA - Hanover, MD - [Cleveland, Ohio]

                    “Enhanced design of turbo-jet LPT by separation control using phased plasma actuators” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

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

                    Online Access

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                      11An edge-based solution-adaptive method applied to the AIRPLANE code

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                      “An edge-based solution-adaptive method applied to the AIRPLANE code” Metadata:

                      • Title: ➤  An edge-based solution-adaptive method applied to the AIRPLANE code
                      • Author:
                      • Language: English
                      • Publisher: ➤  Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: ➤  [Springfield, Va - [Moffett Field, CA]

                      “An edge-based solution-adaptive method applied to the AIRPLANE code” 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

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                        12Solar rocket plume/mirror interactions

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                        “Solar rocket plume/mirror interactions” Metadata:

                        • Title: ➤  Solar rocket plume/mirror interactions
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration
                        • Publish Date:
                        • Publish Location: [Washington, D.C.]

                        “Solar rocket plume/mirror interactions” 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

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                          13Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil

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                          “Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” Metadata:

                          • Title: ➤  Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration - Joint Institute for Aeronautics and Acoustics, Stanford University - National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center
                          • Publish Date:
                          • Publish Location: ➤  [Stanford, Calif.] - [Washington, DC - Springfield, Va

                          “Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil” 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.

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                            14Evaluation of 3D inverse code using rotor 67 as test case

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                            “Evaluation of 3D inverse code using rotor 67 as test case” Metadata:

                            • Title: ➤  Evaluation of 3D inverse code using rotor 67 as test case
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                            • Publish Date:
                            • Publish Location: ➤  Springfield, Va - [Washington, DC

                            “Evaluation of 3D inverse code using rotor 67 as test case” 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

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                              15Experimental aerothermodynamic research of hypersonic aircraft

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                              “Experimental aerothermodynamic research of hypersonic aircraft” Metadata:

                              • Title: ➤  Experimental aerothermodynamic research of hypersonic aircraft
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                              • Publish Date:
                              • Publish Location: ➤  Springfield, Va.? - [Washington, DC

                              “Experimental aerothermodynamic research of hypersonic aircraft” 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

                              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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                                16Effects of winglets on a first-generation jet transport wing

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                                “Effects of winglets on a first-generation jet transport wing” Metadata:

                                • Title: ➤  Effects of winglets on a first-generation jet transport wing
                                • Author:
                                • Language: English
                                • Number of Pages: Median: 56
                                • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Dryden Flight Research Facility
                                • Publish Date:
                                • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Edwards, Calif

                                “Effects of winglets on a first-generation jet transport wing” 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

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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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                                  17Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

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                                  “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:

                                  • Title: ➤  Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
                                  • 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

                                  “Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” 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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                                    18Wing pressure distributions from subsonic tests of a high-wing transport model

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                                    “Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:

                                    • Title: ➤  Wing pressure distributions from subsonic tests of a high-wing transport model
                                    • 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

                                    “Wing pressure distributions from subsonic tests of a high-wing transport model” 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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                                      19Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

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                                      “Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Metadata:

                                      • Title: ➤  Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
                                      • 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: ➤  [Springfield, Va - [Washington, D.C.]

                                      “Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel” 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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                                        20Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing

                                        By

                                        “Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” Metadata:

                                        • Title: ➤  Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
                                        • Publish Date:
                                        • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                        “Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing” 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.

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                                          21Computer code study of asteroid entry into Venusian atmosphere

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                                          “Computer code study of asteroid entry into Venusian atmosphere” Metadata:

                                          • Title: ➤  Computer code study of asteroid entry into Venusian atmosphere
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  Springfield, Va - [Washington, DC

                                          “Computer code study of asteroid entry into Venusian atmosphere” 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

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                                            22Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV

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                                            “Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” Metadata:

                                            • Title: ➤  Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV
                                            • 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, D.C.]

                                            “Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV” 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

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                                              23Calculation of multistage turbomachinery using steady characteristic boundary conditions

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                                              “Calculation of multistage turbomachinery using steady characteristic boundary conditions” Metadata:

                                              • Title: ➤  Calculation of multistage turbomachinery using steady characteristic boundary conditions
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Aeronautics and Space Administration Langley Research Center - Available from National Technical Information Service
                                              • Publish Date:
                                              • Publish Location: ➤  [Cleveland, Ohio] - Springfield, Va

                                              “Calculation of multistage turbomachinery using steady characteristic boundary conditions” 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

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                                                24Atmospheric probe model

                                                By

                                                “Atmospheric probe model” Metadata:

                                                • Title: Atmospheric probe model
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                • Publish Date:
                                                • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                “Atmospheric probe model” 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.

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                                                  25Vibroacoustic response of pad structures to space shuttle launch acoustic loads

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                                                  “Vibroacoustic response of pad structures to space shuttle launch acoustic loads” Metadata:

                                                  • Title: ➤  Vibroacoustic response of pad structures to space shuttle launch acoustic loads
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                  • Publish Date:
                                                  • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                  “Vibroacoustic response of pad structures to space shuttle launch acoustic loads” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1995
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
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                                                    26Coupling of low speed fan stator vane unsteady pressures to duct modes

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                                                    “Coupling of low speed fan stator vane unsteady pressures to duct modes” Metadata:

                                                    • Title: ➤  Coupling of low speed fan stator vane unsteady pressures to duct modes
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
                                                    • Publish Date:
                                                    • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio]

                                                    “Coupling of low speed fan stator vane unsteady pressures to duct modes” Subjects and Themes:

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                                                    • First Year Published: 1999
                                                    • Is Full Text Available: No
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                                                      27An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet

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                                                      “An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Metadata:

                                                      • Title: ➤  An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
                                                      • 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

                                                      “An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Subjects and Themes:

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                                                      • First Year Published: 1997
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
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                                                        28Direct calculation of airfoils from pressure distribution

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                                                        “Direct calculation of airfoils from pressure distribution” Metadata:

                                                        • Title: ➤  Direct calculation of airfoils from pressure distribution
                                                        • Author:
                                                        • Number of Pages: Median: 61
                                                        • Publisher: NASA
                                                        • Publish Date:
                                                        • Publish Location: Washington, D. C

                                                        “Direct calculation of airfoils from pressure distribution” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1974
                                                        • Is Full Text Available: No
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                                                        29Development of a variational SEASAT data analysis technique

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                                                        “Development of a variational SEASAT data analysis technique” Metadata:

                                                        • Title: ➤  Development of a variational SEASAT data analysis technique
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                        • Publish Date:
                                                        • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                        “Development of a variational SEASAT data analysis technique” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

                                                        • First Year Published: 1986
                                                        • Is Full Text Available: No
                                                        • Is The Book Public: No
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                                                          30Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach

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                                                          “Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Metadata:

                                                          • Title: ➤  Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                          • Publish Date:
                                                          • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                          “Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach” Subjects and Themes:

                                                          Edition Identifiers:

                                                          Access and General Info:

                                                          • First Year Published: 1996
                                                          • Is Full Text Available: No
                                                          • Is The Book Public: No
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                                                            31Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

                                                            By

                                                            “Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:

                                                            • Title: ➤  Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
                                                            • Publish Date:
                                                            • Publish Location: Springfield, VA - Hampton, Va

                                                            “Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:

                                                            Edition Identifiers:

                                                            Access and General Info:

                                                            • First Year Published: 1995
                                                            • Is Full Text Available: No
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                                                              32Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

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                                                              “Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Metadata:

                                                              • Title: ➤  Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf
                                                              • 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

                                                              “Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf” Subjects and Themes:

                                                              Edition Identifiers:

                                                              Access and General Info:

                                                              • First Year Published: 1996
                                                              • Is Full Text Available: No
                                                              • Is The Book Public: No
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                                                                33Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel

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                                                                “Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel” Metadata:

                                                                • Title: ➤  Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind tunnel
                                                                • Author:
                                                                • Language: English
                                                                • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                                                • Publish Date:
                                                                • Publish Location: Hampton, Va

                                                                “Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the AEDC 16T propulsion wind 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

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                                                                  34Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel

                                                                  By

                                                                  “Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel” Metadata:

                                                                  • Title: ➤  Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind tunnel
                                                                  • Author:
                                                                  • Language: English
                                                                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
                                                                  • Publish Date:
                                                                  • Publish Location: Hampton, Va

                                                                  “Pressure distributions obtained on a 0.10-scale model of the space shuttle orbiter's forebody in the Ames unitary plan wind 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

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                                                                    35Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure

                                                                    By

                                                                    “Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure” Metadata:

                                                                    • Title: ➤  Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure
                                                                    • Author:
                                                                    • Number of Pages: Median: 16
                                                                    • Publisher: National Aerospace Laboratory
                                                                    • Publish Date:
                                                                    • Publish Location: Chofu, Tokyo, Japan

                                                                    “Transonic airfoil design on the Navier-Stokes equations to attain arbitrarily specified pressure distribution - an iterative procedure” Subjects and Themes:

                                                                    Edition Identifiers:

                                                                    Access and General Info:

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

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                                                                    36Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow

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                                                                    “Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Metadata:

                                                                    • Title: ➤  Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow
                                                                    • Author:
                                                                    • Number of Pages: Median: 26
                                                                    • Publisher: Institute of Aerophysics
                                                                    • Publish Date:
                                                                    • Publish Location: [Downsview, Ont.]

                                                                    “Approximate calculation of the pressure distribution on a rectangular wing oscillating in incompressible flow” Subjects and Themes:

                                                                    Edition Identifiers:

                                                                    Access and General Info:

                                                                    • First Year Published: 1958
                                                                    • Is Full Text Available: No
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                                                                    37Heat transfer and flow on the first stage blade tip of a power generation gas turbine

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                                                                    “Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Metadata:

                                                                    • Title: ➤  Heat transfer and flow on the first stage blade tip of a power generation gas turbine
                                                                    • Author:
                                                                    • Language: English
                                                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
                                                                    • Publish Date:
                                                                    • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                                                                    “Heat transfer and flow on the first stage blade tip of a power generation gas turbine” Subjects and Themes:

                                                                    Edition Identifiers:

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                                                                    • First Year Published: 1999
                                                                    • Is Full Text Available: No
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                                                                      38Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

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                                                                      “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Metadata:

                                                                      • Title: ➤  Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
                                                                      • Author:
                                                                      • Language: English
                                                                      • Number of Pages: Median: 115
                                                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                                                                      • Publish Date:
                                                                      • Publish Location: Hampton, Va - [Springfield, Va

                                                                      “Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds” Subjects and Themes:

                                                                      Edition Identifiers:

                                                                      Access and General Info:

                                                                      • First Year Published: 1988
                                                                      • Is Full Text Available: No
                                                                      • Is The Book Public: No
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                                                                        39Pressures inside a room subjected to sonic boom

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                                                                        “Pressures inside a room subjected to sonic boom” Metadata:

                                                                        • Title: ➤  Pressures inside a room subjected to sonic boom
                                                                        • Author:
                                                                        • Publisher: ➤  Institute for Aerospace Studies
                                                                        • Publish Date:
                                                                        • Publish Location: [Downsview, Ont.]

                                                                        “Pressures inside a room subjected to sonic boom” Subjects and Themes:

                                                                        Edition Identifiers:

                                                                        Access and General Info:

                                                                        • First Year Published: 1977
                                                                        • Is Full Text Available: No
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                                                                        40Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1

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                                                                        “Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Metadata:

                                                                        • Title: ➤  Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1
                                                                        • Author:
                                                                        • Number of Pages: Median: 554
                                                                        • Publisher: Naval Surface Weapons Center
                                                                        • Publish Date:
                                                                        • Publish Location: Silver Spring, Md

                                                                        “Handbook of inviscid sphere-cone flow fields and pressure distributions. Volume 1” Subjects and Themes:

                                                                        Edition Identifiers:

                                                                        Access and General Info:

                                                                        • First Year Published: 1975
                                                                        • Is Full Text Available: No
                                                                        • Is The Book Public: No
                                                                        • Access Status: No_ebook

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                                                                        41Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system

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                                                                        “Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” Metadata:

                                                                        • Title: ➤  Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system
                                                                        • Author:
                                                                        • Language: English
                                                                        • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
                                                                        • Publish Date:
                                                                        • Publish Location: ➤  Hanover, MD - [Cleveland, Ohio]

                                                                        “Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system” 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

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                                                                          42Experimental optimization methods for multi-element airfoils

                                                                          By

                                                                          “Experimental optimization methods for multi-element airfoils” Metadata:

                                                                          • Title: ➤  Experimental optimization methods for multi-element airfoils
                                                                          • Author:
                                                                          • Language: English
                                                                          • Publisher: ➤  Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                          • Publish Date:
                                                                          • Publish Location: ➤  Norfolk, Va - [Washington, DC - Springfield, Va

                                                                          “Experimental optimization methods for multi-element airfoils” 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

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                                                                            43Rapid numerical simulation of viscous axisymmetric flow fields

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                                                                            “Rapid numerical simulation of viscous axisymmetric flow fields” Metadata:

                                                                            • Title: ➤  Rapid numerical simulation of viscous axisymmetric flow fields
                                                                            • Author:
                                                                            • Language: English
                                                                            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                                                            • Publish Date:
                                                                            • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                                                            “Rapid numerical simulation of viscous axisymmetric flow fields” 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

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                                                                              44Analysis of advanced solid rocket motor ignition phenomena

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                                                                              “Analysis of advanced solid rocket motor ignition phenomena” Metadata:

                                                                              • Title: ➤  Analysis of advanced solid rocket motor ignition phenomena
                                                                              • Author:
                                                                              • Language: English
                                                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                              • Publish Date:
                                                                              • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                                              “Analysis of advanced solid rocket motor ignition phenomena” 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

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                                                                                45Performance and pressure data from a small model tilt-rotor in hover

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                                                                                “Performance and pressure data from a small model tilt-rotor in hover” Metadata:

                                                                                • Title: ➤  Performance and pressure data from a small model tilt-rotor in hover
                                                                                • Author:
                                                                                • Language: English
                                                                                • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                                                                • Publish Date:
                                                                                • Publish Location: ➤  [Springfield, Va - Moffett Field, CA

                                                                                “Performance and pressure data from a small model tilt-rotor in hover” 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

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                                                                                  46Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds

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                                                                                  “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:

                                                                                  • Title: ➤  Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
                                                                                  • Author:
                                                                                  • Language: English
                                                                                  • Number of Pages: Median: 51
                                                                                  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
                                                                                  • Publish Date:
                                                                                  • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                                                                  “Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” 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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                                                                                    47Numerical analysis of base flowfield for a four-engine clustered nozzle configuration

                                                                                    By

                                                                                    “Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” Metadata:

                                                                                    • Title: ➤  Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
                                                                                    • Author:
                                                                                    • Language: English
                                                                                    • Publisher: ➤  [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
                                                                                    • Publish Date:
                                                                                    • Publish Location: ➤  Washington, DC - Springfield, Va

                                                                                    “Numerical analysis of base flowfield for a four-engine clustered nozzle configuration” 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

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                                                                                      48Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles

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                                                                                      “Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles” Metadata:

                                                                                      • Title: ➤  Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles
                                                                                      • Author:
                                                                                      • Language: English
                                                                                      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                                                      • Publish Date:
                                                                                      • Publish Location: ➤  Springfield, Va - [Washington, DC

                                                                                      “Study of the kinematic and load sharing properties of wormgearing with non-symmetric tooth profiles” 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

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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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                                                                                        49Interaction of sound from supersonic jets with nearby structures

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                                                                                        “Interaction of sound from supersonic jets with nearby structures” Metadata:

                                                                                        • Title: ➤  Interaction of sound from supersonic jets with nearby structures
                                                                                        • Author:
                                                                                        • Language: English
                                                                                        • Publisher: ➤  National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
                                                                                        • Publish Date:
                                                                                        • Publish Location: [Springfield, Va - Hampton, VA

                                                                                        “Interaction of sound from supersonic jets with nearby structures” 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.

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                                                                                          50Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5

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                                                                                          “Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5” Metadata:

                                                                                          • Title: ➤  Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5
                                                                                          • Author:
                                                                                          • Number of Pages: Median: 58
                                                                                          • Publisher: Langley Research Center
                                                                                          • Publish Date:
                                                                                          • Publish Location: Hampton, Va

                                                                                          “Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5” 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

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                                                                                          Source: Wikipedia

                                                                                          Wikipedia Results

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                                                                                          Pressure coefficient

                                                                                          dynamics, the pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field. The pressure coefficient is

                                                                                          Pressure system

                                                                                          A pressure system is a peak or lull in the sea level pressure distribution, a feature of synoptic-scale weather. The surface pressure at sea level varies

                                                                                          Lift (force)

                                                                                          to tip, and the pressure distributions around the airfoil sections change accordingly in the spanwise direction. Pressure distributions in planes perpendicular

                                                                                          Adverse pressure gradient

                                                                                          in aerodynamics since flow separation significantly modifies the pressure distribution along the surface and hence the lift and drag characteristics. Turbulent

                                                                                          Archimedes' principle

                                                                                          depth distribution, therefore they also have the same pressure distribution, and consequently the same total force resulting from hydrostatic pressure, exerted

                                                                                          Contact patch

                                                                                          vehicle. The size and shape of the contact patch, as well as the pressure distribution within the contact patch, are important to the ride qualities and

                                                                                          Coandă effect

                                                                                          solved in closed form, giving the distribution of velocity along the circular wall. The surface pressure distribution is then calculated using Bernoulli

                                                                                          Pressure

                                                                                          distributed. Gauge pressure (also spelled gage pressure) is the pressure relative to the ambient pressure. Various units are used to express pressure. Some of these

                                                                                          Pore water pressure

                                                                                          Pore water pressures below the phreatic level of the groundwater are measured with piezometers. The vertical pore water pressure distribution in aquifers

                                                                                          Drag (physics)

                                                                                          the boundary layer and pressure distribution over the body surface. Therefore, there are three ways of categorizing drag. Pressure drag and friction drag