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Source: The Open Library

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1Thrust-reverser flow investigation on a twin-engine transport

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“Thrust-reverser flow investigation on a twin-engine transport” Metadata:

  • Title: ➤  Thrust-reverser flow investigation on a twin-engine transport
  • Author:
  • Language: English
  • Number of Pages: Median: 153
  • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

“Thrust-reverser flow investigation on a twin-engine transport” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

Online Access

Downloads Are Not Available:

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

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    2Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows

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    “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Metadata:

    • Title: ➤  Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
    • Author:
    • Language: English
    • Number of Pages: Median: 180
    • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Hampton, Va - [Washington, D.C.]

    “Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” 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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      3Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

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      “Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities” Metadata:

      • Title: ➤  Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities
      • Author:
      • Number of Pages: Median: 106
      • Publisher: NASA
      • Publish Date:
      • Publish Location: Washington

      “Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

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

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      4Why do airlines want and use thrust reversers?

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      “Why do airlines want and use thrust reversers?” Metadata:

      • Title: ➤  Why do airlines want and use thrust reversers?
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: [Springfield, Va - Hampton, Va

      “Why do airlines want and use thrust reversers?” 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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        5Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction

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        “Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction” Metadata:

        • Title: ➤  Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction
        • 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

        “Magellan aerodynamic characteristics during the termination experiment including thruster plume-free stream interaction” 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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          6Static performance of six innovative thrust reverser concepts for subsonic transport applications

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          “Static performance of six innovative thrust reverser concepts for subsonic transport applications” Metadata:

          • Title: ➤  Static performance of six innovative thrust reverser concepts for subsonic transport applications
          • 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

          “Static performance of six innovative thrust reverser concepts for subsonic transport applications” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 2000
          • 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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            7Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

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            “Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Metadata:

            • Title: ➤  Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
            • Publish Date:
            • Publish Location: [Washington, D.C.]

            “Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

            Online Access

            Downloads Are Not Available:

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

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              8Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

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              “Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” Metadata:

              • Title: ➤  Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
              • Publish Date:
              • Publish Location: ➤  [Washington, D.C.] - Springfield, Va

              “Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” 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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                9Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment

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                “Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment” Metadata:

                • Title: ➤  Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment
                • 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, Calif

                “Investigation of wing upper surface flow-field disturbance due to NASA DC-8-72 in-flight inboard thrust-reverser deployment” Subjects and Themes:

                Edition Identifiers:

                Access and General Info:

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

                Online Access

                Downloads Are Not Available:

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

                Online Borrowing:

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                  10Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

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                  “Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers” Metadata:

                  • Title: ➤  Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
                  • Author:
                  • Number of Pages: Median: 40
                  • Publisher: Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va

                  “Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers” 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 Marketplaces

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