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Source: The Open Library

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1Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance

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“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Metadata:

  • Title: ➤  Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1998
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    2Unsteady blade row interaction in a transonic turbine

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    “Unsteady blade row interaction in a transonic turbine” Metadata:

    • Title: ➤  Unsteady blade row interaction in a transonic turbine
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Springfield, Va

    “Unsteady blade row interaction in a transonic turbine” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1996
    • 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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      3Turbomachinery design and tonal acoustics computations

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      “Turbomachinery design and tonal acoustics computations” Metadata:

      • Title: ➤  Turbomachinery design and tonal acoustics computations
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration - MCAT Institute
      • Publish Date:
      • Publish Location: ➤  [Washington, DC - Springfield, Va - San Jose, CA

      “Turbomachinery design and tonal acoustics computations” 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:

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        4Supersonic through-flow fan engine and aircrraft mission performance

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        “Supersonic through-flow fan engine and aircrraft mission performance” Metadata:

        • Title: ➤  Supersonic through-flow fan engine and aircrraft mission performance
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Cleveland, Ohio

        “Supersonic through-flow fan engine and aircrraft mission performance” 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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          5Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade

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          “Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade” Metadata:

          • Title: ➤  Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade
          • Author:
          • Publisher: ➤  von Karman Institute for Fluid Dynamics
          • Publish Date:
          • Publish Location: Rhode Saint Genese, Belgium

          “Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1990
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          De Laval nozzle

          nozzles are widely used in some types of steam turbines and rocket engine nozzles. It also sees use in supersonic jet engines. Similar flow properties have

          Gas turbine

          such as micro turbines and also have strong potential for use in small gas turbines/auxiliary power units A major challenge facing turbine design, especially

          Turbojet

          the combustor expand through the turbine. Typical materials for turbines include inconel and Nimonic. The hottest turbine vanes and blades in an engine have

          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

          Afterburner

          jet engines, mostly those on military supersonic aircraft. Its purpose is to increase thrust, usually for supersonic flight, takeoff, and combat. The afterburning

          Supersonic transport

          A supersonic transport (SST) or a supersonic airliner is a civilian supersonic aircraft designed to transport passengers at speeds greater than the speed

          Components of jet engines

          rotating at independent speeds, with as many sets of turbines and compressors. Cooling air for the turbines may flow through the shaft from the compressor.

          Variable cycle engine

          such as subsonic, transonic and supersonic. An advanced technology engine is a turbine engine that allows different turbines to spin at different, individually

          Supersonic aircraft

          A supersonic aircraft is an aircraft capable of supersonic flight, that is, flying faster than the speed of sound (Mach 1). Supersonic aircraft were developed

          Boom Technology

          Boom Technology, Inc. (trade name Boom Supersonic) is an American company developing the Overture, a supersonic airliner. It has also flight tested a one-third-scale