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Books Results

Source: The Open Library

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Search results from The Open Library

1The art of sharp-leading-edged delta wings with blowing

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“The art of sharp-leading-edged delta wings with blowing” Metadata:

  • Title: ➤  The art of sharp-leading-edged delta wings with blowing
  • Author:
  • Language: English
  • Publisher: ➤  Stanford University, Dept. of Aeronautics and Astronautics - Joint Institute for Aeronautics and Acoustics - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Stanford, CA - [Springfield, Va

“The art of sharp-leading-edged delta wings with blowing” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1985
  • 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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    2Fabrication and testing of a leading-edge-shaped heat pipe

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    “Fabrication and testing of a leading-edge-shaped heat pipe” Metadata:

    • Title: ➤  Fabrication and testing of a leading-edge-shaped heat pipe
    • 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

    “Fabrication and testing of a leading-edge-shaped heat pipe” 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.

    Online Borrowing:

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      3Supersonic leading edge receptivity

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      “Supersonic leading edge receptivity” Metadata:

      • Title: ➤  Supersonic leading edge receptivity
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
      • Publish Date:
      • Publish Location: Hampton, Va - [Springfield, Va

      “Supersonic leading edge receptivity” 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.

      Online Borrowing:

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        4Numerical simulation of leading-edge vortex flow

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        “Numerical simulation of leading-edge vortex flow” Metadata:

        • Title: ➤  Numerical simulation of leading-edge vortex flow
        • Author:
        • Number of Pages: Median: 30
        • Publisher: ➤  National Aerospace Laboratories
        • Publish Date:
        • Publish Location: Amsterdam, Netherlands

        “Numerical simulation of leading-edge vortex flow” 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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        5The lift of sharp-leading-edged delta wings with blowing

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        “The lift of sharp-leading-edged delta wings with blowing” Metadata:

        • Title: ➤  The lift of sharp-leading-edged delta wings with blowing
        • Author:
        • Number of Pages: Median: 17
        • Publisher: ➤  Stanford University, Dept. of Aeronautics and Astronautics
        • Publish Date:
        • Publish Location: Stanford, Calif

        “The lift of sharp-leading-edged delta wings with blowing” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1985
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Marketplaces

        Find The lift of sharp-leading-edged delta wings with blowing at online marketplaces:



        Wiki

        Source: Wikipedia

        Wikipedia Results

        Search Results from Wikipedia

        Kutta–Joukowski theorem

        as for a flat plate, the leading edge is also sharp, then vortices also shed at the leading edge and the role of leading edge vortices is two-fold: 1)

        Leading-edge extension

        normal flight to minimize drag. A dogtooth is a small, sharp zig-zag break in the leading edge of a wing. It is usually used on a swept wing, to generate

        Vortex lift

        of lift due to the action of leading edge vortices. It is generated by wings with highly sweptback, sharp, leading edges (beyond 50 degrees of sweep)

        Leading-edge cuff

        leading-edge cuff is a wing leading-edge modification, usually a lightly drooped outboard leading-edge extension. In most cases of outboard leading-edge

        Airfoil

        rounded leading edge, while those designed for supersonic flight tend to be slimmer with a sharp leading edge. All have a sharp trailing edge. The air

        Shaanxi Y-8

        design problems. The first design flaw was that Y-8 wings have very sharp leading edges, so one wing tends to stall before the other, causing the aircraft

        Sharpness (cutting)

        and to test surfaces for relative sharpness. Some materials in the environment naturally break with extremely fine edges. A notable example is obsidian,

        Lockheed Martin RQ-170 Sentinel

        elements common to stealth engineering, such as zigzag edged landing gear doors and sharp leading edges, and the exhaust is not shielded by the wing. Aviation

        Trailing edge

        exerted by the sharp trailing edge of an aerofoil on the circulation.” Other sharp-edged surfaces that are attached to the trailing edges of wings or control

        Waverider

        pronounced heat dissipation problems. Waveriders generally have sharp noses and sharp leading edges on their wings. The underside shock-surface remains attached