Trapped vortex cavity

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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Details

244 90R, 244 87, B64C 500, B64C 2306

Patent

active

050547208

ABSTRACT:
An airfoil having a trailing edge member pivotally connected to a leading edge member. The trailing edge member having a vortex generating cavity that can be exposed or concealed from a stream of fluid flowing over the outer surface of the members.

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Krall et al., "Wind Tunnel Tests of a Trapped Vortex-High Lift Airfoil", Dept. of Navy, ATC Report No. B-94300/3TR-10, 2-23-72 to 12-23-72.
Williams et al., "A Comprehensive Plan for Helicopter Drag Reduction", Report to 31st National Forum by Ad Hac Comm. on Rotorcraft Drag, May 14-15, 1975.

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