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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 70 ̊

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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 70 ̊” Metadata:

  • Title: ➤  Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
  • Author:
  • Language: English
  • Number of Pages: Median: 140
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  Springfield, VA - Hampton, Va - [Springfield, VA

“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊” 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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2Flow-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.

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    3Effects of winglets on a first-generation jet transport wing

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    “Effects of winglets on a first-generation jet transport wing” Metadata:

    • Title: ➤  Effects of winglets on a first-generation jet transport wing
    • Author:
    • Language: English
    • Number of Pages: Median: 56
    • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service] - Dryden Flight Research Facility
    • Publish Date:
    • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Edwards, Calif

    “Effects of winglets on a first-generation jet transport wing” 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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      4Wing pressure distributions from subsonic tests of a high-wing transport model

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      “Wing pressure distributions from subsonic tests of a high-wing transport model” Metadata:

      • Title: ➤  Wing pressure distributions from subsonic tests of a high-wing transport model
      • 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

      “Wing pressure distributions from subsonic tests of a high-wing transport model” 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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        5Euler technology assessment for preliminary aircraft design

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        “Euler technology assessment for preliminary aircraft design” Metadata:

        • Title: ➤  Euler technology assessment for preliminary aircraft design
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
        • Publish Date:
        • Publish Location: Springfield, VA - Hampton, Va

        “Euler technology assessment for preliminary aircraft design” 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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          6A preliminary look at techniques used to obtain airdata from flight at high angles of attack

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          “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Metadata:

          • Title: ➤  A preliminary look at techniques used to obtain airdata from flight at high angles of attack
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Edwards, Calif

          “A preliminary look at techniques used to obtain airdata from flight at high angles of attack” 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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            7Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept

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            “Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Metadata:

            • Title: ➤  Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
            • Author:
            • Language: English
            • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
            • Publish Date:
            • Publish Location: [Springfield, Va - MSFC, Ala

            “Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” 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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