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Source: The Open Library

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1Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method

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“Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method” Metadata:

  • Title: ➤  Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method
  • Author:
  • Language: English
  • Number of Pages: Median: 181
  • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Washington, D.C.] - [Springfield, Va

“Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method” 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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    2In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)

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    “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:

    • Title: ➤  In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
    • 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: ➤  [Springfield, Va - [Washington, DC]

    “In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” 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 In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) at online marketplaces:


      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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        4Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft

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        “Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft” Metadata:

        • Title: ➤  Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft
        • Author:
        • Language: English
        • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

        “Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1984
        • 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 Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivaties for the X-29A aircraft at online marketplaces:


          5Preliminary flight assessment of the X-29A advanced technology demonstrator

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          “Preliminary flight assessment of the X-29A advanced technology demonstrator” Metadata:

          • Title: ➤  Preliminary flight assessment of the X-29A advanced technology demonstrator
          • Author:
          • Language: English
          • Number of Pages: Median: 11
          • Publisher: ➤  National Technical Information Service] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
          • Publish Date:
          • Publish Location: ➤  Edwards, Calif - Springfield, VA

          “Preliminary flight assessment of the X-29A advanced technology demonstrator” 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

          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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            6A progress report on a programme of research into the aerodynamics, stability and control characteristics of a combat aircraft having a forward swept wing

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            “A progress report on a programme of research into the aerodynamics, stability and control characteristics of a combat aircraft having a forward swept wing” Metadata:

            • Title: ➤  A progress report on a programme of research into the aerodynamics, stability and control characteristics of a combat aircraft having a forward swept wing
            • Author:
            • Number of Pages: Median: 10
            • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
            • Publish Date:
            • Publish Location: Cranfield, Eng

            “A progress report on a programme of research into the aerodynamics, stability and control characteristics of a combat aircraft having a forward swept wing” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1985
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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