Explore: Flight Stability Tests

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Source: The Open Library

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1Low-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

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    2Estimation of aircraft nonlinear unsteady parameters from wind tunnel data

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    “Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Metadata:

    • Title: ➤  Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: Hampton, Va - [Springfield, Va

    “Estimation of aircraft nonlinear unsteady parameters from wind tunnel data” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1998
    • 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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      3Lateral stability analysis for X-29A drop model using system identification methodology

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      “Lateral stability analysis for X-29A drop model using system identification methodology” Metadata:

      • Title: ➤  Lateral stability analysis for X-29A drop model using system identification methodology
      • Author:
      • Language: English
      • Number of Pages: Median: 24
      • Publisher: ➤  National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
      • Publish Date:
      • Publish Location: ➤  [Washington, DC] - [Springfield, Va

      “Lateral stability analysis for X-29A drop model using system identification methodology” 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

      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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        4Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data

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        “Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data” Metadata:

        • Title: ➤  Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va

        “Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data” 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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          5The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206

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          “The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206” Metadata:

          • Title: ➤  The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206
          • Author:
          • Number of Pages: Median: 54
          • Publisher: ➤  National Research Council Canada
          • Publish Date:
          • Publish Location: Ottawa

          “The application of linear maximum likelihood estimation of aerodynamic derivatives for the Bell-205 and Bell-206” 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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