Explore: Wing Planforms

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Source: The Open Library

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1Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes

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“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Metadata:

  • Title: ➤  Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: [Springfield, Va - Hampton, Va

“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” 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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    2A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region

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    “A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” Metadata:

    • Title: ➤  A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service [distributor
    • Publish Date:
    • Publish Location: Springfield, VA - Hampton, Va

    “A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region” 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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      Find A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region at online marketplaces:


      3Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds

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      “Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” Metadata:

      • Title: ➤  Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
      • Author:
      • Language: English
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds” 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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        4Equivalent plate analysis of aircraft wing box structures with general planform geometry

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        “Equivalent plate analysis of aircraft wing box structures with general planform geometry” Metadata:

        • Title: ➤  Equivalent plate analysis of aircraft wing box structures with general planform geometry
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center
        • Publish Date:
        • Publish Location: Hampton, Va

        “Equivalent plate analysis of aircraft wing box structures with general planform geometry” 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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          Find Equivalent plate analysis of aircraft wing box structures with general planform geometry at online marketplaces:



          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          Wing configuration

          The wing configuration or planform of a fixed-wing aircraft (including both gliders and powered aeroplanes) is its arrangement of lifting and related surfaces

          Elliptical wing

          spanwise distribution across the wing. There is no inherent superiority to pure elliptical shapes and wings with other planforms can be optimized to give elliptical

          Delta wing

          A delta wing is a wing shaped in the form of a triangle. It is named for its similarity in shape to the Greek uppercase letter delta (Δ). Although long

          Trapezoidal wing

          In aeronautics, a trapezoidal wing is a straight-edged and tapered wing planform. It may have any aspect ratio and may or may not be swept. The thin, unswept

          Circular wing

          A circular wing is a disc-shaped wing having the outer planform of a circle. If the aircraft has no fuselage or tail the disc-shaped craft is sometimes

          Swept wing

          "Speed Record Again Broken?" Saskatoon Star-Phoenix, 25 September 1953. "Wing Planforms for High-Speed Flight." NACA TN-1033. Retrieved: July 24, 2011. Von

          Messerschmitt Me 210

          proved to have unacceptably poor flight characteristics due to serious wing planform and fuselage design flaws. A large-scale operational testing program

          Wingtip vortices

          wingtip, at the edge of flap devices, or at other abrupt changes in wing planform. Wingtip vortices are associated with induced drag, the imparting of

          Aspect ratio (aeronautics)

          wide wing has a low aspect ratio. Aspect ratio and other features of the planform are often used to predict the aerodynamic efficiency of a wing because

          Flying wing

          wash-out, reducing the angle of attack towards the wing tips, together with a swept-back wing planform. The Dunne D.5 incorporated this principle and its