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1The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil

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“The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil” Metadata:

  • Title: ➤  The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
  • Author:
  • Language: English
  • Number of Pages: Median: 18
  • Publisher: ➤  Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - For sale by the National Technical Information Service
  • Publish Date:
  • Publish Location: ➤  [Washington, D.C.] - Springfield, Va - Hampton, Va

“The NASA Langley laminar-flow-control experiment on a swept, supercritical 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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    2Incompressible boundary-layer stability analysis of LFC experimental data for sub-critical Mach numbers

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    “Incompressible boundary-layer stability analysis of LFC experimental data for sub-critical Mach numbers” Metadata:

    • Title: ➤  Incompressible boundary-layer stability analysis of LFC experimental data for sub-critical Mach numbers
    • Author:
    • Number of Pages: Median: 71
    • Publisher: Langley Research Center
    • Publish Date:
    • Publish Location: Hampton, Va

    “Incompressible boundary-layer stability analysis of LFC experimental data for sub-critical Mach numbers” 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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    Wiki

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    Boundary layer control

    control (LFC) The particular control method required for laminar control depends on Reynolds-number and wing leading edge sweep. Hybrid laminar flow control

    Airbus A350

    laminar flow control (HLFC) on the leading edge of an A350 prototype vertical stabiliser, with passive suction similar to the boundary layer control on

    Northrop X-21

    Northrop X-21A was an experimental aircraft designed to test wings with laminar flow control. It was based on the Douglas WB-66D airframe, with the wing-mounted

    General Dynamics F-16XL

    Bohn-Meyer 1992, pp. 2–3. "Past Projects: F-16XL Ship #2 Supersonic Laminar Flow Control". NASA. 10 May 2017. Archived from the original on 26 November 2022

    Laminar Flow (album)

    Laminar Flow is an album by the American musician Roy Orbison. It was recorded at Wishbone Recording Studio in Muscle Shoals, Alabama, and released on

    Laminar flow cabinet

    A laminar flow cabinet or tissue culture hood is a partially enclosed bench work surface designed to prevent contamination of biological samples, semiconductor

    Laminar–turbulent transition

    In fluid dynamics, the process of a laminar flow becoming turbulent is known as laminar–turbulent transition. The main parameter characterizing transition

    Laminar flow reactor

    A laminar flow reactor (LFR) is a type of chemical reactor that uses laminar flow to control reaction rate, and/or reaction distribution. LFR is generally

    Douglas B-66 Destroyer

    designed to conduct laminar flow control studies. Laminar-flow control was thought to potentially reduce drag by as much as 25%. Control would be by removal

    Mass flow sensor

    generations. Laminar flow elements measure the volumetric flow of gases directly. They operate on the principle that, given laminar flow, the pressure


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