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Jimmy L Pittman
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Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
Jimmy L Pittman · National Aeronautics and Space Administration, Scientific and Technical Information Branch
113 sayfa · 1980
Aerodynamics, Supersonic / Hypersonic planes / Mach number / Supersonic Aerodynamics / Supersonic wind tunnels
Body and canard effects on an attached-flow maneuver wing at Mach 1.62
Jimmy L Pittman · For sale by the National Technical Information Service]
145 sayfa · 1984
Aerodynamics, Supersonic / Airplanes / Canard Wings / Supersonic Aerodynamics / Wings, Canard
Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation
Jimmy L. Pittman · For sale by the National Technical Information Service]
Sayfa sayısı yok · 1986
Aerodynamics, Supersonic / Airplanes / Supersonic Aerodynamics / Wings
Application of supersonic linear theory and hypersonic impact methods to three nonslender hypersonic airplane concepts at mach numbers from 1.10 to 2.86
Jimmy L Pittman · For sale by the National Technical Information Service]
56 sayfa · 1979
Mathematical models / Airplanes / Aerodynamics