Airfoil with thick trailing edge

Stock material or miscellaneous articles – Structurally defined web or sheet – Including variation in thickness

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Details

428192, 428212, 244123, 244124, B32B 300, B64C 100

Patent

active

052523810

ABSTRACT:
An airfoil section comprising a relatively thick trailing edge and a sloped rear surface.

REFERENCES:
patent: 1710672 (1929-04-01), Bonney
patent: 3504873 (1970-04-01), Spence
patent: 4560358 (1985-12-01), Adler
Sighard Hoerner, et al., Fluid-Dynamic Drag, 1965, pp. 3-22.
P. A. Henne et al., A New Airfoil Design Concept, American Institute of Aeronautics and Astronautics, Inc. 1989.
Abbott and Von Doenhoff, Theory of Wing Sections, Dover Publications, 1959, pp. 228 and 229.

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