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Source: The Open Library

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1A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

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“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” Metadata:

  • Title: ➤  A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” 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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    2Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

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    “Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:

    • Title: ➤  Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

    “Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” 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.

    Online Borrowing:

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      33D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

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      “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:

      • Title: ➤  3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, DC]

      “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” 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.

      Online Borrowing:

        Online Marketplaces

        Find 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:


        4Factors affecting the performance of supersonic diffusers

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        “Factors affecting the performance of supersonic diffusers” Metadata:

        • Title: ➤  Factors affecting the performance of supersonic diffusers
        • Author:
        • Number of Pages: Median: 22
        • Publisher: ➤  [Institute of Aerophysics] - Institute of Aerophysics
        • Publish Date:
        • Publish Location: [Downsview, Ont.]

        “Factors affecting the performance of supersonic diffusers” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1952
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        53D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

        By

        “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:

        • Title: ➤  3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” 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.

        Online Borrowing:

          Online Marketplaces

          Find 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:


          6Further tests with a variable ramp intake having a design Mach number of 2.2

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          “Further tests with a variable ramp intake having a design Mach number of 2.2” Metadata:

          • Title: ➤  Further tests with a variable ramp intake having a design Mach number of 2.2
          • Author:
          • Language: English
          • Publisher: H.M.S.O.
          • Publish Date:
          • Publish Location: London

          “Further tests with a variable ramp intake having a design Mach number of 2.2” Subjects and Themes:

          Edition Identifiers:

          • The Open Library ID: OL6016955M
          • Online Computer Library Center (OCLC) ID: 6157431
          • Library of Congress Control Number (LCCN): 66075050

          Access and General Info:

          • First Year Published: 1966
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          7Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

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          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:

          • Title: ➤  Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
          • Author:
          • Language: English
          • Number of Pages: Median: 37
          • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
          • Publish Date:
          • Publish Location: Washington - Springfield, Va

          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

          Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:


          8Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

          By

          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:

          • Title: ➤  Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
          • Author:
          • Language: English
          • Number of Pages: Median: 37
          • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
          • Publish Date:
          • Publish Location: Springfield, Va - Washington

          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

          Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:


          9Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41

          By

          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:

          • Title: ➤  Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
          • Author:
          • Language: English
          • Number of Pages: Median: 37
          • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
          • Publish Date:
          • Publish Location: Springfield, Va - Washington

          “Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

          Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:


          10Supersonic diffusors for large pressure recovery

          By

          “Supersonic diffusors for large pressure recovery” Metadata:

          • Title: ➤  Supersonic diffusors for large pressure recovery
          • Author:
          • Number of Pages: Median: 88
          • Publisher: ➤  Dept. of Aeronautical Engineering, University of Toronto
          • Publish Date:
          • Publish Location: Toronto

          “Supersonic diffusors for large pressure recovery” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1948
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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          11Supersonic inlets

          By

          “Supersonic inlets” Metadata:

          • Title: Supersonic inlets
          • Author:
          • Language: English
          • Number of Pages: Median: 158
          • Publisher: ➤  North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
          • Publish Date:
          • Publish Location: [Paris]

          “Supersonic inlets” Subjects and Themes:

          Edition Identifiers:

          • The Open Library ID: OL5531016M
          • Online Computer Library Center (OCLC) ID: 1838021
          • Library of Congress Control Number (LCCN): 67006377

          Access and General Info:

          • First Year Published: 1965
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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