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1Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel

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“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” Metadata:

  • Title: ➤  Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel
  • 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

“Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel” 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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    2A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel

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    “A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” Metadata:

    • Title: ➤  A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Astronautics and Aeronautics
    • Publish Date:
    • Publish Location: ➤  Reston, VA - [Washington, D.C - Springfield, Va

    “A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” 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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      3Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction

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      “Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” Metadata:

      • Title: ➤  Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - Center for Aerodynamics Research, Dept. of Aerospace Engineering & Engineering Mechanics, University of Texas at Austin - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - Austin, Tex - [Washington, DC

      “Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction” 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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        4Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results

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        “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:

        • Title: ➤  Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: Hampton, Va - Springfield, VA

        “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” 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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        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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          5Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer

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          “Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer” Metadata:

          • Title: ➤  Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer
          • Author:
          • Publisher: ➤  [Institute for Aerospace Studies] - Institute for Aerospace Studies
          • Publish Date:
          • Publish Location: [Downsview, Ont.]

          “Quantitative laser Schlieren measurements in an expanding hypersonic laminar boundary layer” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1971
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          6The investigation of the structure of hypersonic turbulent boundary layers on a 5 degree sharp cone using the electron beam fluorescence technique

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          “The investigation of the structure of hypersonic turbulent boundary layers on a 5 degree sharp cone using the electron beam fluorescence technique” Metadata:

          • Title: ➤  The investigation of the structure of hypersonic turbulent boundary layers on a 5 degree sharp cone using the electron beam fluorescence technique
          • Author:
          • Number of Pages: Median: 26
          • Publisher: ➤  Imperial College of Science and Technology
          • Publish Date:
          • Publish Location: London

          “The investigation of the structure of hypersonic turbulent boundary layers on a 5 degree sharp cone using the electron beam fluorescence technique” 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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          7Hypersonic turbulent boundary-layer and free shear database

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          “Hypersonic turbulent boundary-layer and free shear database” Metadata:

          • Title: ➤  Hypersonic turbulent boundary-layer and free shear database
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

          “Hypersonic turbulent boundary-layer and free shear database” 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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            8On the Mach number independence principle for a hypersonic boundary layer

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            “On the Mach number independence principle for a hypersonic boundary layer” Metadata:

            • Title: ➤  On the Mach number independence principle for a hypersonic boundary layer
            • Author:
            • Number of Pages: Median: 13
            • Publisher: ➤  Princeton University, Dept. of Aeronautical Engineering
            • Publish Date:
            • Publish Location: Princeton, N. J

            “On the Mach number independence principle for a hypersonic boundary layer” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1959
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            9Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers

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            “Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers” Metadata:

            • Title: ➤  Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C - Springfield, Va

            “Turbulence measurements in hypersonic boundary layers using contant-temperature anemometry and Reynolds stress measurements in hypersonic boundary layers” 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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              10On the instability of hypersonic flow past a flat plate

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              “On the instability of hypersonic flow past a flat plate” Metadata:

              • Title: ➤  On the instability of hypersonic flow past a flat plate
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “On the instability of hypersonic flow past a flat plate” 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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                11Crossflow effects on the growth rate of inviscid Gortler vortices in a hypersonic boundary layer

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                “Crossflow effects on the growth rate of inviscid Gortler vortices in a hypersonic boundary layer” Metadata:

                • Title: ➤  Crossflow effects on the growth rate of inviscid Gortler vortices in a hypersonic boundary layer
                • Author:
                • Number of Pages: Median: 34
                • Publisher: ➤  Institute for Computer Applications in Science and Engineering
                • Publish Date:
                • Publish Location: Hampton Va

                “Crossflow effects on the growth rate of inviscid Gortler vortices in a hypersonic boundary layer” 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

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