Explore: Vortex Flaps

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Books Results

Source: The Open Library

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1Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane

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“Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” Metadata:

  • Title: ➤  Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane
  • Author:
  • Language: English
  • Number of Pages: Median: 35
  • Publisher: ➤  For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office - Langley Research Center
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va - Hampton, Va

“Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” 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.

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    2Vortex flow aerodynamics, volume I

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    “Vortex flow aerodynamics, volume I” Metadata:

    • Title: ➤  Vortex flow aerodynamics, volume I
    • Author:
    • Number of Pages: Median: 395
    • Publisher: Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Vortex flow aerodynamics, volume I” 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

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    3Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms

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    “Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Metadata:

    • Title: ➤  Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information - National Technical Information Service [distributor
    • Publish Date:
    • Publish Location: ➤  Springfield, VA - Hanover, MD - Hampton, Va

    “Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • 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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      4Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing

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      “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing” Metadata:

      • Title: ➤  Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing
      • Author:
      • Number of Pages: Median: 25
      • Publisher: ➤  Cranfield Institute of Technology, College of Aeronautics
      • Publish Date:
      • Publish Location: Cranfield, Bedford, England

      “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing” 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

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      5Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing

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      “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Metadata:

      • Title: ➤  Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
      • Author:
      • Number of Pages: Median: 16
      • Publisher: National Aerospace Laboratory
      • Publish Date:
      • Publish Location: Tokyo

      “Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Subjects and Themes:

      Edition Identifiers:

      Access and General Info:

      • First Year Published: 1992
      • Is Full Text Available: No
      • Is The Book Public: No
      • Access Status: No_ebook

      Online Marketplaces

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      6Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap

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      “Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap” Metadata:

      • Title: ➤  Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap
      • Author:
      • Number of Pages: Median: 309
      • Publisher: Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap” 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 Marketplaces

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      7The behaviour and performance of leading edge vortex flaps

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      “The behaviour and performance of leading edge vortex flaps” Metadata:

      • Title: ➤  The behaviour and performance of leading edge vortex flaps
      • Author:
      • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
      • Publish Date:
      • Publish Location: Cranfield, U.K

      “The behaviour and performance of leading edge vortex flaps” 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

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      8Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps

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      “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Metadata:

      • Title: ➤  Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
      • Author:
      • Number of Pages: Median: 44
      • Publisher: Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va

      “Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” 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 Marketplaces

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      Wiki

      Source: Wikipedia

      Wikipedia Results

      Search Results from Wikipedia

      Vortex generator

      effectiveness of wings and control surfaces, such as flaps, elevators, ailerons, and rudders. Vortex generators are most often used to delay flow separation

      High-lift device

      Flaps are usually located on the trailing edge of a wing, while leading edge flaps are used occasionally. There are many kinds of trailing-edge flap.

      Vortex lift

      behaviour and performance of leading-edge Vortex flaps" (PDF). Retrieved 2023-12-17. "Leading Edge Vortex Allows Bats to Stay Aloft, Aerospace Professor

      Gurney flap

      to the wing without the flaps. Storms, B. L.; Jang, C. S. (1994). "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators". Journal of

      Blown flap

      Blown flaps, blown wing or jet flaps are powered aerodynamic high-lift devices used on the wings of certain aircraft to improve their low-speed flight

      Flap (aeronautics)

      trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance and the landing distance. Flaps also cause an increase in drag so they

      Wingtip vortices

      configuration of the flaps could be changed on existing aircraft to break the vortex into three smaller and less disturbing vortexes. This primarily involved

      Insect flight

      Stollery, J. L. (1988). "The Behaviour and Performance of Leading-Edge Vortex Flaps" (PDF). ICAS 1988 Jerusalem. 1988. International Council of Aeronautical

      Krueger flap

      Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. Unlike slats or droop flaps, the

      Leading-edge slat

      and trailing-edge ailerons (i.e. what would later be called trailing-edge flaps) that could be deployed in conjunction with the leading-edge slats to test