Aeronautics and astronautics – Aircraft structure – Details
Patent
1986-09-19
1988-04-12
Barefoot, Galen
Aeronautics and astronautics
Aircraft structure
Details
244207, 244119, B64C 2104
Patent
active
047369132
ABSTRACT:
A fluid flow control device controllably maintains attached flow in the region of a body having a contour of rapid curvature utilizing tangential fluid discharge slots, positioned just upstream from the separation line, which issue a thin jet sheet to energize the boundary layer and entrain the surrounding flow. When applied to the aft fuselage of an aircraft, the device reduces separation and vortex drag at cruise and provides control forces and moments during low speed operation of the aircraft.
REFERENCES:
patent: 2041791 (1936-05-01), Stalker
patent: 3066894 (1962-12-01), Davidson
patent: 3419232 (1968-12-01), McStay et al.
patent: 3807662 (1974-04-01), Velazquez
Bennett John A.
Englar Robert J.
Thomas Andrew S. W.
Barefoot Galen
Katz Eric R.
Lockheed Corporation
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