Explore: Dynamic Stability

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Source: The Open Library

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1Heave instabilities of amphibious air cushion suspension systems

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“Heave instabilities of amphibious air cushion suspension systems” Metadata:

  • Title: ➤  Heave instabilities of amphibious air cushion suspension systems
  • Author:
  • Publisher: ➤  Institute for Aerospace Studies
  • Publish Date:
  • Publish Location: [Downsview, Ont.]

“Heave instabilities of amphibious air cushion suspension systems” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1979
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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2High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test

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“High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” Metadata:

  • Title: ➤  High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
  • Publish Date:
  • Publish Location: ➤  Edwards, Calif - [Springfield, Va

“High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” 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

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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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    3Bibliography on determination of supersonic dynamic stability derivatives

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    “Bibliography on determination of supersonic dynamic stability derivatives” Metadata:

    • Title: ➤  Bibliography on determination of supersonic dynamic stability derivatives
    • Author: ➤  
    • Number of Pages: Median: 38
    • Publisher: ➤  National Aeronautical Establishment
    • Publish Date:
    • Publish Location: Ottawa, Ont

    “Bibliography on determination of supersonic dynamic stability derivatives” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1966
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    4Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane

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    “Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane” Metadata:

    • Title: ➤  Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane
    • Author:
    • Number of Pages: Median: 57
    • Publisher: Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Wind-tunnel static and free-flight investigation of high-angle-of attack stability and control characteristics of a model of the EA-6B airplane” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1992
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

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    5Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors

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    “Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors” Metadata:

    • Title: ➤  Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: Washington, D.C

    “Experimental determination of gap flow-conditioned forces at turbine stages and their effect on the running stability of simple rotors” 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

    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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      6Analysis of wind tunnel oscillatory data of the X-31A aircraft

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      “Analysis of wind tunnel oscillatory data of the X-31A aircraft” Metadata:

      • Title: ➤  Analysis of wind tunnel oscillatory data of the X-31A aircraft
      • 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

      “Analysis of wind tunnel oscillatory data of the X-31A aircraft” 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.

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        7Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration

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        “Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration” Metadata:

        • Title: ➤  Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration
        • Author:
        • Number of Pages: Median: 32
        • Publisher: Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va

        “Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1989
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

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        8Dynamic response and stability of a composite prop-fan model

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        “Dynamic response and stability of a composite prop-fan model” Metadata:

        • Title: ➤  Dynamic response and stability of a composite prop-fan model
        • Author:
        • Language: English
        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Lewis Research Center
        • Publish Date:
        • Publish Location: ➤  Cleveland, Ohio - [Springfield, Va

        “Dynamic response and stability of a composite prop-fan model” 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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          9High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test

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          “High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” Metadata:

          • Title: ➤  High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - [Springfield, Va

          “High-angle-of-attack yawing movement asymmetry of the X-31 aircraft from flight test” 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.

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            10Subsonic dynamics of stardust sample return capsule

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            “Subsonic dynamics of stardust sample return capsule” Metadata:

            • Title: ➤  Subsonic dynamics of stardust sample return capsule
            • 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

            “Subsonic dynamics of stardust sample return capsule” 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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              11Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps

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              “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Metadata:

              • Title: ➤  Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
              • Author:
              • Number of Pages: Median: 44
              • Publisher: Langley Research Center
              • Publish Date:
              • Publish Location: Hampton, Va

              “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” 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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              12V/STOL dynamics, control, and flying qualities

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              “V/STOL dynamics, control, and flying qualities” Metadata:

              • Title: ➤  V/STOL dynamics, control, and flying qualities
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for AeroSpace Information
              • Publish Date:
              • Publish Location: ➤  Hanover, MD - Moffett Field, Calif

              “V/STOL dynamics, control, and flying qualities” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 2000
              • 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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