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    Design of a Slotted, Natural-Laminar-Flow Airfoil for Business-Jet Applications (2012)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: A 14-percent-thick, slotted, natural-laminar-flow airfoil, the S204, for light business-jet applications has been designed and analyzed theoretically. The two primary objectives of high maximum lift, relatively insensitive to roughness, and low profile drag have been achieved. The drag-divergence Mach number is predicted to be greater than 0.70.
    Keywords: Aerodynamics
    Type: NASA/CR-2012-217559 , NF1676L-14320
    Format: application/pdf
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