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Source: The Open Library

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1Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor

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“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” Metadata:

  • Title: ➤  Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - [Washington, DC]

“Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor” 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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    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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      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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        4Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A

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        “Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” Metadata:

        • Title: ➤  Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center
        • Publish Date:
        • Publish Location: [Cleveland, Ohio

        “Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A” 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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          5Fundamental study of flow field generated by rotorcraft blades

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          “Fundamental study of flow field generated by rotorcraft blades” Metadata:

          • Title: ➤  Fundamental study of flow field generated by rotorcraft blades
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  Pasadena, Calif - [Springfield, Va

          “Fundamental study of flow field generated by rotorcraft blades” 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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            6Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions

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            “Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions” Metadata:

            • Title: ➤  Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - [Washington, DC]

            “Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff 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.

            Online Borrowing:

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              Find Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions at online marketplaces: