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Source: The Open Library

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1Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle

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“Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle” Metadata:

  • Title: ➤  Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle
  • Author:
  • Language: English
  • Number of Pages: Median: 51
  • Publisher: ➤  Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, D.C.]

“Flow analysis and design optimization methods for nozzle afterbody of a hypersonic vehicle” Subjects and Themes:

Edition Identifiers:

Access and General Info:

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

Online Access

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    2Validation of the NPARC code for nozzle afterbody flows at transonic speeds

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    “Validation of the NPARC code for nozzle afterbody flows at transonic speeds” Metadata:

    • Title: ➤  Validation of the NPARC code for nozzle afterbody flows at transonic speeds
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

    “Validation of the NPARC code for nozzle afterbody flows at transonic speeds” 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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      3Experimental 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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        4Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

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        “Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” Metadata:

        • Title: ➤  Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
        • Author:
        • Language: English
        • Number of Pages: Median: 120
        • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
        • Publish Date:
        • Publish Location: ➤  Edwards, Calif - [Springfield, Va - [Washington, DC]

        “Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds” 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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          5Computational design aspects of a NASP nozzle/afterbody experiment

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          “Computational design aspects of a NASP nozzle/afterbody experiment” Metadata:

          • Title: ➤  Computational design aspects of a NASP nozzle/afterbody experiment
          • Author:
          • Number of Pages: Median: 14
          • Publisher: ➤  American Institute of Aeronautics and Astronautics
          • Publish Date:
          • Publish Location: Washington, D. C

          “Computational design aspects of a NASP nozzle/afterbody experiment” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

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          6Transonic Navier-Stokes solutions of three-dimensional afterbody flows

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          “Transonic Navier-Stokes solutions of three-dimensional afterbody flows” Metadata:

          • Title: ➤  Transonic Navier-Stokes solutions of three-dimensional afterbody flows
          • Author:
          • Number of Pages: Median: 58
          • Publisher: Langley Research Center
          • Publish Date:
          • Publish Location: Hampton, Va

          “Transonic Navier-Stokes solutions of three-dimensional afterbody flows” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

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          7Computational assessment of aft-body closure for the HSR reference H configuration

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          “Computational assessment of aft-body closure for the HSR reference H configuration” Metadata:

          • Title: ➤  Computational assessment of aft-body closure for the HSR reference H configuration
          • 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

          “Computational assessment of aft-body closure for the HSR reference H configuration” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

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

          Online Access

          Downloads Are Not Available:

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

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            8Interference on a model afterbody from downstream support hardware at transonic Mach numbers

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            “Interference on a model afterbody from downstream support hardware at transonic Mach numbers” Metadata:

            • Title: ➤  Interference on a model afterbody from downstream support hardware at transonic Mach numbers
            • Author:
            • Number of Pages: Median: 48
            • Publisher: ➤  Arnold Engineering Development Center/DOT, Air Force Systems Command
            • Publish Date:
            • Publish Location: Arnold Air Force Station, Tenn

            “Interference on a model afterbody from downstream support hardware at transonic Mach numbers” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

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

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            9Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes

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            “Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes” Metadata:

            • Title: ➤  Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C - Springfield, Va

            “Exhausted plume flow field prediction near the afterbody of hypersonic flight vehicles in high altitudes” 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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              10The effect of exhaust plume/afterbody interaction on installed scramjet performance

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              “The effect of exhaust plume/afterbody interaction on installed scramjet performance” Metadata:

              • Title: ➤  The effect of exhaust plume/afterbody interaction on installed scramjet performance
              • Author:
              • Language: English
              • Number of Pages: Median: 95
              • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

              “The effect of exhaust plume/afterbody interaction on installed scramjet performance” 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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