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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

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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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    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.

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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:

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        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:

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          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

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          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

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          “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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          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          Diffuser (thermodynamics)

          important role in a supersonic diffuser. Diffusers are very common in heating, ventilating, and air-conditioning systems. Diffusers are used in both all-air

          Compressible flow

          aircraft inlet design, objects in supersonic flight, and (at a more fundamental level) supersonic nozzles and diffusers. Depending on the flow conditions

          Ramjet

          engine to provide air for combustion. Ramjets work most efficiently at supersonic speeds around Mach 3 (2,300 mph; 3,700 km/h) and can operate up to Mach 6

          Inlet cone

          (sometimes called shock cones or inlet centerbodies) are a component of some supersonic aircraft and missiles. They are primarily used on ramjets, such as the

          Scramjet

          A scramjet (supersonic combustion ramjet) is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in

          Arthur Kantrowitz

          propulsion were published in 1988. His early research included supersonic diffusers and supersonic compressors in the early 40s, which has since been applied

          Diffuser

          Look up diffuser or diffusers in Wiktionary, the free dictionary. Diffuser may refer to: Diffuser (automotive), a shaped section of a car's underbody

          Unstart

          In supersonic aerodynamics, an unstart refers to a generally violent breakdown of the supersonic airflow. The phenomenon occurs when mass flow rate changes

          Nozzle

          distribution of air via ceiling diffusers is not possible or not practical. Diffusers that uses jet nozzles are called jet diffuser where it will be arranged

          Kantrowitz limit

          Arthur; duP, Coleman (May 1945). "Preliminary Investigation of Supersonic Diffusers" (PDF). Advance Confidential Report L5D20. Archived (PDF) from the