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    Boundary layer crossflow stabilization of high subsonic speed LFC transport airplanes (1988)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: With a view to the elaboration of the design of Mach 0.83 and 0.97 cruise-speed long-range aircraft employing LFC, a study is conducted of the laminar flow characteristics of supercritical airfoils of blunt leading-edge X88 type, for the case of lightly loaded wings that dispense with leading-edge flaps for low-speed operations. The boundary layer crossflow in the front acceleration zone of these airfoils' upper surface is optimally stabilized by suction in the upstream portion of the zone, yielding a crossflow that is neutrally stable.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 88-0275
    Format: text
    Location Call Number Expected Availability
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