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Source: The Open Library

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1Nozzle thrust optimization while reducing jet noise

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“Nozzle thrust optimization while reducing jet noise” Metadata:

  • Title: ➤  Nozzle thrust optimization while reducing jet noise
  • Author:
  • Language: English
  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C - Springfield, Va

“Nozzle thrust optimization while reducing jet noise” 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

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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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    2A control-volume method for analysis of unsteady thrust augmenting ejector flows

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    “A control-volume method for analysis of unsteady thrust augmenting ejector flows” Metadata:

    • Title: ➤  A control-volume method for analysis of unsteady thrust augmenting ejector flows
    • Author:
    • Language: English
    • Publisher: ➤  Lewis Research Center, National Aeronautics and Space Administration - For sale by the National Technical Information Service
    • Publish Date:
    • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

    “A control-volume method for analysis of unsteady thrust augmenting ejector flows” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1988
    • 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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      3Thrust augmentation measurements using a pulse detonation engine ejector

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      “Thrust augmentation measurements using a pulse detonation engine ejector” Metadata:

      • Title: ➤  Thrust augmentation measurements using a pulse detonation engine ejector
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service [distributor - Available from NASA Center for Aerospace Information
      • Publish Date:
      • Publish Location: ➤  [Cleveland, Ohio] - Springfield, VA - Hanover, MD

      “Thrust augmentation measurements using a pulse detonation engine ejector” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 2003
      • 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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        4A design study of hydrazine and biowaste resistojets

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        “A design study of hydrazine and biowaste resistojets” Metadata:

        • Title: ➤  A design study of hydrazine and biowaste resistojets
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

        “A design study of hydrazine and biowaste resistojets” 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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          5Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle

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          “Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” Metadata:

          • Title: ➤  Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

          “Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” 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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            6Unsteady ejector performance

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            “Unsteady ejector performance” Metadata:

            • Title: Unsteady ejector performance
            • Author:
            • Language: English
            • Publisher: ➤  Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Glenn Research Center
            • Publish Date:
            • Publish Location: Cleveland, Ohio - Hanover MD

            “Unsteady ejector performance” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 2002
            • 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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