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Source: The Open Library

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1Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

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“Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel” Metadata:

  • Title: ➤  Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel
  • 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

“Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel” 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

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    2Rocket-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:

    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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      3Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel

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

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

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

      Edition Identifiers:

      Access and General Info:

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

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      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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        4Study of CFD methods applied to rapidly deforming boundaries

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        “Study of CFD methods applied to rapidly deforming boundaries” Metadata:

        • Title: ➤  Study of CFD methods applied to rapidly deforming boundaries
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, D.C

        “Study of CFD methods applied to rapidly deforming boundaries” 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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          5Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows

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          “Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows” Metadata:

          • Title: ➤  Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - [Springfield, Va

          “Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows” 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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            6Static presssure position error calibration of the NAE T-33 C-FSKH

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            “Static presssure position error calibration of the NAE T-33 C-FSKH” Metadata:

            • Title: ➤  Static presssure position error calibration of the NAE T-33 C-FSKH
            • Author:
            • Number of Pages: Median: 33
            • Publisher: ➤  National Aeronautical Establishment
            • Publish Date:
            • Publish Location: Ottawa

            “Static presssure position error calibration of the NAE T-33 C-FSKH” 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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            7The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers

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            “The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers” Metadata:

            • Title: ➤  The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - National Technical Information Service, distributor]
            • Publish Date:
            • Publish Location: ➤  [Washington, DC] - [Springfield, Va

            “The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Access

            Downloads Are Not Available:

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

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              8Experimental cavity pressure measurements at subsonic and transonic speeds

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              “Experimental cavity pressure measurements at subsonic and transonic speeds” Metadata:

              • Title: ➤  Experimental cavity pressure measurements at subsonic and transonic speeds
              • Author:
              • Number of Pages: Median: 73
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Experimental cavity pressure measurements at subsonic and transonic speeds” 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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              9A preliminary look at techniques used to obtain airdata from flight at high angles of attack

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              “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Metadata:

              • Title: ➤  A preliminary look at techniques used to obtain airdata from flight at high angles of attack
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - Edwards, Calif

              “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

              Online Access

              Downloads Are Not Available:

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

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                10Analysis of fluctuating static pressure measurements in the National Transonic Facility

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                “Analysis of fluctuating static pressure measurements in the National Transonic Facility” Metadata:

                • Title: ➤  Analysis of fluctuating static pressure measurements in the National Transonic Facility
                • Author:
                • Number of Pages: Median: 180
                • Publisher: Langley Research Center
                • Publish Date:
                • Publish Location: Hampton, Va

                “Analysis of fluctuating static pressure measurements in the National Transonic Facility” 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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                11Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)

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                “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” Metadata:

                • Title: ➤  Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)
                • Author:
                • Language: English
                • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                • Publish Date:
                • Publish Location: ➤  Springfield, Va - [Washington, DC

                “Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)” 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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                  12Method for determining the time delay of the pitot-static tubing system of aircraft

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                  “Method for determining the time delay of the pitot-static tubing system of aircraft” Metadata:

                  • Title: ➤  Method for determining the time delay of the pitot-static tubing system of aircraft
                  • Author:
                  • Number of Pages: Median: 16
                  • Publisher: National Aerospace Laboratory
                  • Publish Date:
                  • Publish Location: Amsterdam

                  “Method for determining the time delay of the pitot-static tubing system of aircraft” 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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                  13PSP measurement of stator vane surface pressures in a high speed fan

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                  “PSP measurement of stator vane surface pressures in a high speed fan” Metadata:

                  • Title: ➤  PSP measurement of stator vane surface pressures in a high speed fan
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
                  • Publish Date:
                  • Publish Location: ➤  [Cleveland, Ohio] - [Springfield, Va

                  “PSP measurement of stator vane surface pressures in a high speed fan” 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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                    14A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

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                    “A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” Metadata:

                    • Title: ➤  A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
                    • Publish Date:
                    • Publish Location: Hampton, Va - [Springfield, Va

                    “A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92” 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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                      15Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel

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                      “Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” Metadata:

                      • Title: ➤  Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
                      • Author:
                      • Language: English
                      • Publisher: ➤  Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
                      • Publish Date:
                      • Publish Location: Hampton, Va - Hanover, MD

                      “Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” 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

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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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