Aeronautics and astronautics – Aircraft structure – Details
Patent
1986-12-29
1988-12-06
Barefoot, Galen
Aeronautics and astronautics
Aircraft structure
Details
2961801, 2961804, B64C 138
Patent
active
047891173
ABSTRACT:
A body adapted to move downstream through a fluid has a downstream extending smooth surface terminating at a blunt base. A plurality of adjacent U-shaped, downstream extending troughs in the smooth surface intersect the blunt base to form trough outlets. The troughs are appropriately spaced apart, sized and configured to flow full over their entire length and cause fluid to flow into the space immediately behind the blunt base, thereby reducing base drag on the body.
REFERENCES:
patent: 1366635 (1921-01-01), Conway
patent: 2074201 (1937-03-01), Bechereau
patent: 2238749 (1941-04-01), Peltier
patent: 2962101 (1960-11-01), Vaghi
patent: 3072368 (1963-01-01), Seddon et al.
patent: 3434425 (1969-03-01), Critcher
patent: 3481531 (1969-12-01), MacArthur et al.
patent: 3776363 (1973-12-01), Kuethe
patent: 3873048 (1975-03-01), Platou
patent: 4343506 (1982-08-01), Saltzman
"Axisymmetric Bluff Body Drag Reduction Through Geometrical Modification", by Howard and Doodman, Journal of Aircraft, vol. 22, #6, 6/85.
"Longitudinal Grooves for Bluff Body Drag Reduction", by Howard, Quass, Weinstein and Bushnell, AIAA Technical Note 81-4095, vol. 19, No. 4, Apr. 1981.
Paterson Robert W.
Presz, Jr. Walter M.
Werle Michael J.
Barefoot Galen
Corl Rodney
Revis Stephen E.
United Technologies Corporation
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