Explore: Turboprop Aircraft

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Source: The Open Library

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Search results from The Open Library

1Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers

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“Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers” Metadata:

  • Title: ➤  Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers
  • Author:
  • Number of Pages: Median: 112
  • Publisher: Langley Research Center
  • Publish Date:
  • Publish Location: Hampton, Va

“Low-speed aerodynamic characteristics of a twin-engine general aviation configuration with aft-fuselage-mounted pusher propellers” 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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2An estimate of the enroute noise of an advanced turboprop airplane

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“An estimate of the enroute noise of an advanced turboprop airplane” Metadata:

  • Title: ➤  An estimate of the enroute noise of an advanced turboprop airplane
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
  • Publish Date:
  • Publish Location: Cleveland, Ohio

“An estimate of the enroute noise of an advanced turboprop airplane” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1986
  • 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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    3Laboratory experiments on active suppression of advanced tuboprop noise

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    “Laboratory experiments on active suppression of advanced tuboprop noise” Metadata:

    • Title: ➤  Laboratory experiments on active suppression of advanced tuboprop noise
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
    • Publish Date:
    • Publish Location: [Cleveland, Ohio

    “Laboratory experiments on active suppression of advanced tuboprop noise” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1985
    • 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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      4Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft

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      “Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft” Metadata:

      • Title: ➤  Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft
      • Author:
      • Number of Pages: Median: 145
      • Publisher: Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Development and testing of cabin sidewall acoustic resonators for the reduction of cabin tone levels in propfan-powered aircraft” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1991
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

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      5Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration

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      “Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration” Metadata:

      • Title: ➤  Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration
      • Author:
      • Number of Pages: Median: 47
      • Publisher: Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Low-speed wind-tunnel investigation of the flight dynamic characteristics of an advanced turboprop business/commuter aircraft configuration” 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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      6Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)

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      “Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)” Metadata:

      • Title: ➤  Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)
      • Author:
      • Language: English
      • Number of Pages: Median: 23
      • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

      “Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)” 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

      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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        7Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions

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        “Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions” Metadata:

        • Title: ➤  Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions
        • Author:
        • Language: English
        • Number of Pages: Median: 23
        • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  Springfield, Va - [Washington, D.C.]

        “Noise of a simulated installed model counter rotation propeller at angle-of-attack and takeoff/approach conditions” 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

        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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          8Civil tiltrotor feasibility study for the New York and Washington terminal areas

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          “Civil tiltrotor feasibility study for the New York and Washington terminal areas” Metadata:

          • Title: ➤  Civil tiltrotor feasibility study for the New York and Washington terminal areas
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
          • Publish Date:
          • Publish Location: Hanover, MD - Hampton, Va

          “Civil tiltrotor feasibility study for the New York and Washington terminal areas” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 2001
          • 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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            9Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications

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            “Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” Metadata:

            • Title: ➤  Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: Hampton, Va - [Springfield, Va

            “Anaylsis of interior noise ground and flight test data for advanced turboprop aircraft applications” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1991
            • 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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              10Evaluation of installed performance of a wing-tip-mounted pusher turboprop of a semispan wing

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              “Evaluation of installed performance of a wing-tip-mounted pusher turboprop of a semispan wing” Metadata:

              • Title: ➤  Evaluation of installed performance of a wing-tip-mounted pusher turboprop of a semispan wing
              • Author:
              • Number of Pages: Median: 27
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Evaluation of installed performance of a wing-tip-mounted pusher turboprop of a semispan wing” 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 Marketplaces

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