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Sterling C. Evans Library & Annex Library
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
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Miller, David S.
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1
Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /
Published 1981
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2
Body and canard effects on an attached-flow maneuver wing at Mach 1.62 /
by
Pittman, Jimmy L.
Published 1984
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3
Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept /
by
Wood, Richard M.
Published 1983
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4
Experimental investigation of leading-edge thrust at supersonic speeds /
by
Wood, Richard M.
Published 1983
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5
Wing planform effects at supersonic speeds for an advanced fighter configuration /
by
Wood, Richard M.
Published 1984
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6
Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations /
by
Wood, Richard M.
Published 1984
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7
Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds /
by
Covell, Peter F.
Published 1987
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8
Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation /
by
Pittman, Jimmy L.
Published 1984
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9
Lee-side flow over delta wings at supersonic speeds /
by
Miller, David S.
Published 1985
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Miller, David S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Wood, Richard M.
6 results
6
Mason, William H. (William Henry), 1947-
2 results
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Pittman, Jimmy L.
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Brentner, Kenneth S.
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Covell, Peter F.
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Langley Research Center
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English
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United States
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