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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:

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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:

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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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                      Wiki

                      Source: Wikipedia

                      Wikipedia Results

                      Search Results from Wikipedia

                      Kantrowitz limit

                      area, that a hypersonic inlet can employ while successfully starting an engine inlet (or avoiding the expelling of the hypersonic inlet shock wave). The

                      Rocket-based combined cycle

                      Thruster, Demonstrating Tri-Fluid Rocket Injector Capabilities - SpaceRef Hypersonic inlet studies for a small-scale rocket-based combined-cycle engine, Journal

                      Lockheed Martin SR-72

                      Martin SR-72, commonly referred to as "Son of Blackbird," is an American hypersonic concept intended for intelligence, surveillance, and reconnaissance (ISR)

                      SABRE (rocket engine)

                      Engine) was a concept under development by Reaction Engines Limited for a hypersonic precooled hybrid air-breathing rocket engine. The engine was designed

                      Boeing X-51 Waverider

                      Waverider is an unmanned research scramjet experimental aircraft for hypersonic flight at Mach 5 (3,300 mph; 5,300 km/h) and an altitude of 70,000 feet

                      Shcramjet

                      is a concept of air-breathing ramjet engine, proposed to be used for hypersonic and/or single-stage-to-orbit propulsion applications. The shcramjet engine

                      Oblique shock

                      design of supersonic aircraft engine intakes or supersonic inlets. A type of these inlets is wedge-shaped to compress air flow into the combustion chamber

                      Compressible flow

                      Mach 3, the XB-70 used rectangular inlets with adjustable ramps and the SR-71 used circular inlets with adjustable inlet cone. Incompressible flow Conservation

                      YJ-15

                      China's first hypersonic cruise missile". South China Moring Post. Pryhodko, Roman (17 August 2025). "China to Demonstrate New Hypersonic and Supersonic

                      Supersonic transport

                      "This hypersonic airliner would take you from Los Angeles to Tokyo in under two hours". NBC News. August 23, 2019. Tegler, Eric. "Swiss Hypersonic Startup