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    Wind tunnel testing of low-drag airfoils (1986)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Results are presented for the measured performance recently obtained on several airfoil concepts designed to achieve low drag by maintaining extensive regions of laminar flow without compromising high-lift performance. The wind tunnel results extend from subsonic to transonic speeds and include boundary-layer control through shaping and suction. The research was conducted in the NASA Langley 8-Ft Transonic Pressure Tunnel (TPT) and Low Turbulence Pressure Tunnel (LTPT) which have been developed for testing such low-drag airfoils. Emphasis is placed on identifying some of the major factors influencing the anticipated performance of low-drag airfoils.
    Keywords: AERODYNAMICS
    Type: Laminar Flow Aircraft Certification; p 89-128
    Format: application/pdf
    Location Call Number Expected Availability
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