Explore: Variable Sweep Wings

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Source: The Open Library

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1An aerodynamic tradeoff study of the scissor wing configuration

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“An aerodynamic tradeoff study of the scissor wing configuration” Metadata:

  • Title: ➤  An aerodynamic tradeoff study of the scissor wing configuration
  • Author:
  • Language: English
  • Publisher: ➤  University of Missouri-Rolla - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Hampton, Va - Rolla, Mo

“An aerodynamic tradeoff study of the scissor wing 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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    2Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I

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    “Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I” Metadata:

    • Title: ➤  Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I
    • Author:
    • Language: English
    • Number of Pages: Median: 63
    • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service]
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Edwards, Calif

    “Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I” 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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      Find Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I at online marketplaces:


      3Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

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      “Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825” Metadata:

      • Title: ➤  Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - Edwards, Calif

      “Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825” 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.

      Online Borrowing:

        Online Marketplaces

        Find Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 at online marketplaces:


        4Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79

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        “Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79” Metadata:

        • Title: ➤  Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - For sale by the National Technical Information Service
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Edwards, Calif

        “Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79” 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.

        Online Borrowing:

          Online Marketplaces

          Find Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 at online marketplaces:


          5Flutter clearance of the F-14A variable-sweep transition flight experiment airplane

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          “Flutter clearance of the F-14A variable-sweep transition flight experiment airplane” Metadata:

          • Title: ➤  Flutter clearance of the F-14A variable-sweep transition flight experiment airplane
          • Author:
          • Language: English
          • Number of Pages: Median: 39
          • 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

          “Flutter clearance of the F-14A variable-sweep transition flight experiment airplane” 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.

          Online Borrowing:

            Online Marketplaces

            Find Flutter clearance of the F-14A variable-sweep transition flight experiment airplane at online marketplaces:


            6Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow

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            “Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow” Metadata:

            • Title: ➤  Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow
            • Author:
            • Number of Pages: Median: 225
            • Publisher: Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va

            “Wind-tunnel investigation of aerodynamic characteristics and wing pressure distributions of an airplane with variable-sweep wings modified for laminar flow” 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 Marketplaces

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            7Classical dynamics of variable sweep wing aircraft

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            “Classical dynamics of variable sweep wing aircraft” Metadata:

            • Title: ➤  Classical dynamics of variable sweep wing aircraft
            • Author:
            • Number of Pages: Median: 147
            • Publisher: ➤  Dept. of Aerospace Engineering, Indian Institute of Science
            • Publish Date:
            • Publish Location: Bangalore, India

            “Classical dynamics of variable sweep wing aircraft” 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 Marketplaces

            Find Classical dynamics of variable sweep wing aircraft at online marketplaces:


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