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Source: The Open Library

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1Shock-tunnel combustor testing for hypersonic vehicles

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“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:

  • Title: ➤  Shock-tunnel combustor testing for hypersonic vehicles
  • Author:
  • Language: English
  • Publisher: ➤  MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - San Jose, Calif - [Washington, DC

“Shock-tunnel combustor testing for hypersonic vehicles” 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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    23-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions

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    “3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions” Metadata:

    • Title: ➤  3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer interactions
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

    “3-D Navier-Stokes analysis of crossing, glancing shocks/turbulent boundary layer 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

    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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      3Numerical simulation of supersonic and hypersonic inlet flow fields

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      “Numerical simulation of supersonic and hypersonic inlet flow fields” Metadata:

      • Title: ➤  Numerical simulation of supersonic and hypersonic inlet flow fields
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - Mars Mission Research Center, North Carolina State University
      • Publish Date:
      • Publish Location: ➤  [Washington, DC - Raleigh, N.C - Springfield, Va

      “Numerical simulation of supersonic and hypersonic inlet 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

      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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        4Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

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        “Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” Metadata:

        • Title: ➤  Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code” 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

        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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          5Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

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          “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:

          • Title: ➤  Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
          • 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

          “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” 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

          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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            6Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

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            “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:

            • Title: ➤  Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
            • 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

            “Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” 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

            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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              7Computational analysis in support of the SSTO flowpath test

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              “Computational analysis in support of the SSTO flowpath test” Metadata:

              • Title: ➤  Computational analysis in support of the SSTO flowpath test
              • Author:
              • Language: English
              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
              • Publish Date:
              • Publish Location: ➤  [Washington, DC] - [Springfield, Va

              “Computational analysis in support of the SSTO flowpath test” 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

              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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                8Computational modeling and validation for hypersonic inlets

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                “Computational modeling and validation for hypersonic inlets” Metadata:

                • Title: ➤  Computational modeling and validation for hypersonic inlets
                • Author:
                • Language: English
                • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                • Publish Date:
                • Publish Location: ➤  [Washington, D.C - Springfield, Va

                “Computational modeling and validation for hypersonic inlets” 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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                  9A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field

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                  “A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Metadata:

                  • Title: ➤  A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - North Carolina State University
                  • Publish Date:
                  • Publish Location: ➤  Springfield, Va - Raleligh, NC - [Washington, DC

                  “A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1991
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  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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                    10Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10

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                    “Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” Metadata:

                    • Title: ➤  Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center - NASA Center for AeroSpace Information, distributor
                    • Publish Date:
                    • Publish Location: ➤  Springfield, Va - Hampton, Va - Linthicum Heights, MD

                    “Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10” 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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