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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

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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    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.

    Online Borrowing:

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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.

      Online Borrowing:

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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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