Download Effects of sting support interference on the base pressures of a model having a blunt nosed cylinder body and a conical flare at Mach numbers of 0.65 to 2.20
Аthor: Reese, D. E., Jr., Wehrend, W. R., Jr
Formаts: pdf, android, audio, epub, text, ebook, ipad
Total size: 7.96 MB
ІSВN: 1990001080801
Dаtе: 10.07.2012
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experimental investigation of the aerodynamics of a wing in a slipstream . an experimental study of a wing in a propeller slipstream was made in order to determine
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Full text of "Handbook of rock excavation, methods and cost"
Effects of sting support interference on the base pressures of a model having a blunt nosed cylinder body and a conical flare at Mach numbers of 0.65 to 2.20
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