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Source: The Open Library

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1Control & 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

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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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    2An investigation of bleed configurations and their effect on shock wave/boundary layer interactions

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    “An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” Metadata:

    • Title: ➤  An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - University of Cincinnati - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Cincinnati, Ohio?] - [Washington, DC

    “An investigation of bleed configurations and their effect on shock wave/boundary layer interactions” 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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      3A numerical method for solving the three-dimensional parabolized Navier-Stokes equations

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      “A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” Metadata:

      • Title: ➤  A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
      • Author:
      • Language: English
      • Publisher: ➤  Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: Hampton, VA - [Springfield, Va

      “A numerical method for solving the three-dimensional parabolized Navier-Stokes equations” 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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          5Stability of the laminar boundary layer in a streamwise corner

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          “Stability of the laminar boundary layer in a streamwise corner” Metadata:

          • Title: ➤  Stability of the laminar boundary layer in a streamwise corner
          • Author:
          • Language: English
          • Publisher: ➤  Old Dominion University Research Foundation - National Aeronautics and Space Administration, Langley Research Center
          • Publish Date:
          • Publish Location: Norfolk, Va - Hampton, Va

          “Stability of the laminar boundary layer in a streamwise corner” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1984
          • 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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            6An investigation of the flow characteristics in the blade endwall corner region

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            “An investigation of the flow characteristics in the blade endwall corner region” Metadata:

            • Title: ➤  An investigation of the flow characteristics in the blade endwall corner region
            • Author:
            • Number of Pages: Median: 276
            • Publisher: Lewis Research Center
            • Publish Date:
            • Publish Location: Cleveland, Ohio

            “An investigation of the flow characteristics in the blade endwall corner region” 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

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            7Numerical calculations of shock-wave/boundary-layer flow interactions

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            “Numerical calculations of shock-wave/boundary-layer flow interactions” Metadata:

            • Title: ➤  Numerical calculations of shock-wave/boundary-layer flow interactions
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

            “Numerical calculations of shock-wave/boundary-layer flow interactions” 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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              8Supersonic expansion flow of an ionized gas

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              “Supersonic expansion flow of an ionized gas” Metadata:

              • Title: ➤  Supersonic expansion flow of an ionized gas
              • Author:
              • Publisher: ➤  Institute for Aerospace Studies
              • Publish Date:
              • Publish Location: [Downsview, Ont.]

              “Supersonic expansion flow of an ionized gas” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1970
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

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              9Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

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              “Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel” Metadata:

              • Title: ➤  Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
              • Author:
              • Number of Pages: Median: 142
              • Publisher: Lewis Research Center
              • Publish Date:
              • Publish Location: Cleveland, Ohio

              “Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel” 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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              10Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel

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              “Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel” Metadata:

              • Title: ➤  Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel
              • Author:
              • Number of Pages: Median: 148
              • Publisher: Lewis Research Center
              • Publish Date:
              • Publish Location: Cleveland, Ohio

              “Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel” 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

              Find Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel at online marketplaces:


              11Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen

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              “Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen” Metadata:

              • Title: ➤  Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen
              • Author:
              • Number of Pages: Median: 124
              • Publisher: DFVLR
              • Publish Date:
              • Publish Location: Koln

              “Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen” 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 Marketplaces

              Find Theoretische und experimentelle Untersuchungen zur Stossreflexion in dreidimensionalen, stationaren, kegeligen Uberschallstromungen at online marketplaces:


              12Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel

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              “Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel” Metadata:

              • Title: ➤  Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel
              • Author:
              • Number of Pages: Median: 51
              • Publisher: Lewis Research Center
              • Publish Date:
              • Publish Location: Cleveland, Ohio

              “Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel” 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

              Find Experimental evaluation of turning vane designs for high-speed and coupled fan-drive corners of 0.1-scale model of NASA Lewis Research Center's proposed Altitude Wind Tunnel at online marketplaces:



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