Explore: Cold Flow Tests

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Source: The Open Library

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1Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube

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“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” Metadata:

  • Title: ➤  Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, D.C

“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” 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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    2Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets

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    “Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Metadata:

    • Title: ➤  Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va - Springfield, VA

    “Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • 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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      3Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream

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      “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:

      • Title: ➤  Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

      “Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” 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.

      Online Borrowing:

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        Find Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream at online marketplaces:


        4Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations

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        “Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Metadata:

        • Title: ➤  Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
        • 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

        “Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” 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.

        Online Borrowing:

          Online Marketplaces

          Find Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations at online marketplaces:


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