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George C Ashby
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Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium
George C. Ashby · National Aeronautics and Space Administration
60 sayfa · 1977
Pressure / Hypersonic wind tunnels / Measurement
A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
George C Ashby · National Aeronautics and Space Administration, Scientific and Technical Information Branch
31 sayfa · 1980
Aerodynamics, Supersonic / Sonic boom / Supersonic Aerodynamics
Near-field sonic-boom pressure signatures for the space shuttle launch and orbiter vehicles at Mach 6
George C Ashby · for sale by the National Technical Information Service
33 sayfa · 1979
Reusable space vehicles / Sonic boom
Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium
George C Ashby · National Aeronautics and Space Administration
60 sayfa · 1977
Pressure / Hypersonic wind tunnels / Measurement
Pressure distributions on a 0.02-scale space shuttle orbiter nose at Mach 21.5 in helium
George C. Ashby · National Technical Information Service, distributor
Sayfa sayısı yok · 1994
Space shuttles