Explore: Wing Tips

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Source: The Open Library

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1Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods

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“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Metadata:

  • Title: ➤  Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
  • Author:
  • Language: English
  • Number of Pages: Median: 18
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - [Springfield, VA

“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” 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

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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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    2Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications

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    “Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Metadata:

    • Title: ➤  Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Washington, DC - Norfolk, Va - Springfield, Va

    “Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” 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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      3Turbulence measurements in the near field of a wingtip vortex

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      “Turbulence measurements in the near field of a wingtip vortex” Metadata:

      • Title: ➤  Turbulence measurements in the near field of a wingtip vortex
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

      “Turbulence measurements in the near field of a wingtip vortex” 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:

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        4NACA 0015 wing pressure and trailing vortex measurements

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        “NACA 0015 wing pressure and trailing vortex measurements” Metadata:

        • Title: ➤  NACA 0015 wing pressure and trailing vortex measurements
        • Author:
        • Language: English
        • Publisher: ➤  National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - Washington, D.C

        “NACA 0015 wing pressure and trailing vortex measurements” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1991
        • 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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          5Further developments of the fringe-imaging skin friction technique

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          “Further developments of the fringe-imaging skin friction technique” Metadata:

          • Title: ➤  Further developments of the fringe-imaging skin friction technique
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

          “Further developments of the fringe-imaging skin friction technique” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1996
          • 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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            6Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex

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            “Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex” Metadata:

            • Title: ➤  Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex
            • Author:
            • Language: English
            • Number of Pages: Median: 22
            • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
            • Publish Date:
            • Publish Location: Hampton, Va - [Springfield, Va

            “Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex” 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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              Wiki

              Source: Wikipedia

              Wikipedia Results

              Search Results from Wikipedia

              Wing tip

              A wing tip (or wingtip) is the part of the wing that is most distant from the fuselage of a fixed-wing aircraft. Because the wing tip shape influences

              Wingtip device

              intended to improve the efficiency of fixed-wing aircraft by reducing drag. Although there are several types of wing tip devices which function in different manners

              Wing configuration

              Ju 87 Stuka dive bomber. Cranked or canted tip: tip section dihedral differs from the main wing. The tips may have upwards dihedral as on the F-4 Phantom

              Brogue shoe

              The brogue (from Scottish Gaelic bròg and Irish Gaelic bróg, both meaning "shoe") is a style of low-heeled shoe or boot traditionally characterised by

              Forward-swept wing

              the wing tips to such an extent that the tips stall first and one of the main characteristics of the design is lost, on a conventional wing the tips always

              Stall (fluid dynamics)

              stalls before the tip. However, when taken beyond stalling incidence the tips may still become fully stalled before the inner wing despite initial separation

              Wingtip vortices

              left behind a wing as it generates lift. The name is a misnomer because the cores of the vortices are slightly inboard of the wing tips. Wingtip vortices

              Lift (force)

              three-dimensional wing involves significant additional issues, especially relating to the wing tips. For a wing of low aspect ratio, such as a typical delta wing, two-dimensional

              Closed wing

              closed wing is a wing that effectively has two main planes that merge at their ends so that there are no conventional wing tips. Closed wing designs

              Delta wing

              name "Delta", used a very gentle angle so that the wing appeared almost straight and the wing tips had to be cropped sharply (see below). His first such