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Source: The Open Library

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1Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

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“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” Metadata:

  • Title: ➤  Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
  • Author:
  • Language: English
  • Number of Pages: Median: 48
  • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - Langley Research Center
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

“Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil” 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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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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    2Viper

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    “Viper” Metadata:

    • Title: Viper
    • Author:
    • Language: English
    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
    • Publish Date:
    • Publish Location: ➤  Springfield, Va - [Washington, DC

    “Viper” 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 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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      3Two experimental supercritical laminar-flow-control swept-wing airfoils

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      “Two experimental supercritical laminar-flow-control swept-wing airfoils” Metadata:

      • Title: ➤  Two experimental supercritical laminar-flow-control swept-wing airfoils
      • Author:
      • Language: English
      • Number of Pages: Median: 22
      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
      • Publish Date:
      • Publish Location: [Springfield, Va - Hampton, Va

      “Two experimental supercritical laminar-flow-control swept-wing airfoils” 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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        4A summary of transonic natural laminar flow airfoil development at NAE

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        “A summary of transonic natural laminar flow airfoil development at NAE” Metadata:

        • Title: ➤  A summary of transonic natural laminar flow airfoil development at NAE
        • Author:
        • Number of Pages: Median: 120
        • Publisher: ➤  National Aeronautical Establishment
        • Publish Date:
        • Publish Location: Ottawa

        “A summary of transonic natural laminar flow airfoil development at NAE” 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

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        5An approach to the constrained design of natural laminar flow airfoils

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        “An approach to the constrained design of natural laminar flow airfoils” Metadata:

        • Title: ➤  An approach to the constrained design of natural laminar flow airfoils
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  [Washington, D.C - Springfield, Va

        “An approach to the constrained design of natural laminar flow airfoils” 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

        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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          6A boundary-layer transition model for the Navier-Stokes computation for a natural-laminar-flow airfoil

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          “A boundary-layer transition model for the Navier-Stokes computation for a natural-laminar-flow airfoil” Metadata:

          • Title: ➤  A boundary-layer transition model for the Navier-Stokes computation for a natural-laminar-flow airfoil
          • Author:
          • Number of Pages: Median: 20
          • Publisher: National Aerospace Laboratory
          • Publish Date:
          • Publish Location: Tokyo

          “A boundary-layer transition model for the Navier-Stokes computation for a natural-laminar-flow airfoil” 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

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          7Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range

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          “Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range” Metadata:

          • Title: ➤  Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range
          • Author:
          • Number of Pages: Median: 16
          • Publisher: AIAA
          • Publish Date:
          • Publish Location: Washington, D. C

          “Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range” 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

          Find Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range at online marketplaces:


          8Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds

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          “Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds” Metadata:

          • Title: ➤  Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds
          • Author:
          • Number of Pages: Median: 31
          • Publisher: ➤  National Aeronautical Establishment, National Research Council Canada
          • Publish Date:
          • Publish Location: Ottawa

          “Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1988
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

          Find Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds at online marketplaces:



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          Wiki

          Source: Wikipedia

          Wikipedia Results

          Search Results from Wikipedia

          Airfoil

          slowly shock the supersonic flow back to subsonic speeds. Generally such transonic airfoils and also the supersonic airfoils have a low camber to reduce

          Laminar flow

          the concept of the laminar boundary layer to airfoils in 1904. An everyday example is the slow, smooth and optically transparent flow of shallow water over

          Boundary layer control

          fluid is accelerated and thus the point of separation is delayed. Laminar flow airfoils were developed in the 1930s by shaping to maintain a favourable

          NACA airfoil

          Supercritical airfoils designed to independently maximize laminar flow above and below the wing. The numbering is identical to the 7-series airfoils except that

          Reynolds number

          Reynolds numbers, flows tend to be dominated by laminar (sheet-like) flow, while at high Reynolds numbers, flows tend to be turbulent. The turbulence results

          Bell P-63 Kingcobra

          in the application of laminar flow airfoils. In an effort to learn more about the practical application of laminar flow airfoils, in 1945 the Royal Aircraft

          Supercritical airfoil

          rule NACA airfoil Vought F-8 Crusader (TF-8A) Harris, Charles (March 1990). "NASA Supercritical Airfoils: A Matrix of Family-Related Airfoils" (PDF). NASA

          Piaggio P.180 Avanti

          of my career. The laminar flow airfoils were very clean sheet. I think they were the first of the new breed of laminar flow airfoils that demonstrated

          FMA IA 54 Carancho

          glider was to test Dr. Reimar Horten's previous work exploring laminar-flow airfoils, and only one prototype was ever built. The IA 54 was also made

          Flow separation

          layer will be laminar or turbulent can be made by calculating the Reynolds number of the local flow conditions. Separation occurs in flow that is slowing


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