Explore: Guide Vanes

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Source: The Open Library

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1Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels

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“Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels” Metadata:

  • Title: ➤  Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels
  • Author:
  • Language: English
  • Number of Pages: Median: 66
  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
  • Publish Date:
  • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

“Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1989
  • 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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    2Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers

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    “Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” Metadata:

    • Title: ➤  Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

    “Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” 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 Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers at online marketplaces:


      3Experimental 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

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      4Basic fluid mechanics and hydraulic machines

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      Book's cover

      “Basic fluid mechanics and hydraulic machines” Metadata:

      • Title: ➤  Basic fluid mechanics and hydraulic machines
      • Author:
      • Language: English
      • Number of Pages: Median: 234
      • Publisher: BS Publications
      • Publish Date:
      • Publish Location: Hyderabad [India]

      “Basic fluid mechanics and hydraulic machines” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2008
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: Unclassified

      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

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