Explore: Rotor Speed

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Source: The Open Library

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1Helicopter main-rotor speed effects on far-field acoustic levels

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“Helicopter main-rotor speed effects on far-field acoustic levels” Metadata:

  • Title: ➤  Helicopter main-rotor speed effects on far-field acoustic levels
  • Author:
  • Language: English
  • Number of Pages: Median: 18
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center, [Springfield, Va. - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: Hampton, Va

“Helicopter main-rotor speed effects on far-field acoustic levels” 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

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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    2Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations

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    “Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” Metadata:

    • Title: ➤  Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Washington, DC]

    “Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations” 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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      3Performance optimization of a rotor alone Nacelle for acoustic fan testing

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      “Performance optimization of a rotor alone Nacelle for acoustic fan testing” Metadata:

      • Title: ➤  Performance optimization of a rotor alone Nacelle for acoustic fan testing
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
      • Publish Date:
      • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA

      “Performance optimization of a rotor alone Nacelle for acoustic fan testing” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2000
      • 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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        4Tiltrotor vibration reduction through higher harmonic control

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        “Tiltrotor vibration reduction through higher harmonic control” Metadata:

        • Title: ➤  Tiltrotor vibration reduction through higher harmonic control
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, D.C

        “Tiltrotor vibration reduction through higher harmonic control” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1997
        • 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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          5Wide speed range turboshaft study

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          “Wide speed range turboshaft study” Metadata:

          • Title: ➤  Wide speed range turboshaft study
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Washington, D.C - Springfield, Va

          “Wide speed range turboshaft study” 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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            Wiki

            Source: Wikipedia

            Wikipedia Results

            Search Results from Wikipedia

            Helicopter rotor

            On a helicopter, the main rotor or rotor system is the combination of several rotary wings (rotor blades) with a control system, that generates the aerodynamic

            Rotor (electric)

            counterclockwise. Squirrel-cage rotor This rotor rotates at a speed less than the stator rotating magnetic field or synchronous speed. Rotor slip provides necessary

            Variable speed wind turbine

            variable speed wind turbine is one which is specifically designed to operate over a wide range of rotor speeds. It is in direct contrast to fixed speed wind

            Helicopter flight controls

            rotor speed on smaller helicopters without governors. The governors also help the pilot control the collective pitch on the helicopter's main rotors,

            Tiltrotor

            rotor design, with a few exceptions that use other multirotor layouts. Tiltrotor design combines the VTOL capability of a helicopter with the speed and

            Helicopter

            single main rotor and a single tail rotor. Although most earlier designs used more than one main rotor, the configuration of a single main rotor accompanied

            Induction motor

            The rotor accelerates until the magnitude of induced rotor current and torque balances the load on the rotor. Since rotation at synchronous speed does

            Tip-speed ratio

            R} , where ω {\displaystyle \omega } is the rotational speed of the rotor and R is the rotor radius. Therefore, we can also write: λ = ω R v , {\displaystyle

            Squirrel-cage rotor

            stator and the currents in the rotor produce a torque on the rotor. By adjusting the shape of the bars in the rotor, the speed-torque characteristics of the

            Autorotation

            the main rotor to continue turning even if the engine is not running, as well as aerodynamic forces of relative wind maintaining rotor speed. It is the