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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      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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        Wiki

        Source: Wikipedia

        Wikipedia Results

        Search Results from Wikipedia

        Turbine

        performance of a turbine stage. Gas exits the stationary turbine nozzle guide vanes at absolute velocity Va1. The rotor rotates at velocity U. Relative to

        General Electric GEnx

        GE90-94B, shrouded guide vanes reduce secondary flows and counter-rotating spools for the reaction turbines reduce load on guide vanes. To reduce maintenance

        Variable-geometry turbocharger

        done with the use of adjustable vanes located inside the turbine housing between the inlet and turbine, these vanes affect flow of gases towards the

        Turbofan

        turbine nozzle guide vanes would have to be different from the original. In all probability, the downstream LP turbine nozzle guide vanes would have to

        Turbojet

        propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine (that drives the compressor)

        Cross-flow turbine

        two shaped guide vanes. These divide and direct the flow so that the water enters the runner smoothly for any width of opening. The guide vanes should seal

        General Electric J79

        compressor, with one row of variable inlet guide vanes (VIGV's) followed by 6 rows of variable stator vanes Combustors: cannular Turbine: 3-stage Fuel

        Uriah A. Boyden

        conical approach passage for the incoming water—submerged diffusers, guide vanes and a diverting exit passage. Uriah was also the younger brother of Seth

        General Electric J73

        designation was J47-21, but with innovative features including variable inlet guide vanes, double-shell (inner and outer) combustor case, and 50% greater airflow

        Air Algérie Flight 6289

        nozzle guide vanes (stator blades) had been severely damaged, particularly on the lower part of the engine. As some parts of the guide vanes were destroyed