Explore: Stabilizers (fluid Dynamics)

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Source: The Open Library

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1Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept

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“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:

  • Title: ➤  Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
  • Author:
  • Language: English
  • Number of Pages: Median: 23
  • Publisher: ➤  Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Springfield, VA - Hampton, Va

“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” 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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    2Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

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    “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:

    • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
    • Author:
    • Language: English
    • Number of Pages: Median: 145
    • Publisher: ➤  National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  Hampton, Va - [Washington, DC - Springfield, Va

    “Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” 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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      3Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model

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      “Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:

      • Title: ➤  Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - Edwards, Calif

      “Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1994
      • 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 Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model at online marketplaces:


        4DC-10 composite vertical stabilizer ground test program

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        “DC-10 composite vertical stabilizer ground test program” Metadata:

        • Title: ➤  DC-10 composite vertical stabilizer ground test program
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, DC]

        “DC-10 composite vertical stabilizer ground test program” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1983
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        5Some buffet response characteristics of a twin-vertical-tail configuration

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        “Some buffet response characteristics of a twin-vertical-tail configuration” Metadata:

        • Title: ➤  Some buffet response characteristics of a twin-vertical-tail configuration
        • 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

        “Some buffet response characteristics of a twin-vertical-tail 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

        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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          6Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

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          “Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Metadata:

          • Title: ➤  Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
          • Publish Date:
          • Publish Location: ➤  [Washington, DC] - [Springfield, Va

          “Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1993
          • 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 Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 at online marketplaces:


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