Pressure Measurements on Rigid Model of Ballute Decelerator at Mach Numbers from 0.56 to 1.96
1966
16 pages
Report
No indication
English
Aerodynamics , Ballute , Decelerator , Pressure measurement , Rigid structure , Transonic wind tunnel , Drag , Mach number , Measurement , Model , Pressure , Reynolds number , Rigid , Structure , Transonic , Tunnel , Wake , Wind
LOW DENSITY SUPERSONIC DECELERATOR BALLUTE DESIGN AND PACKING
British Library Conference Proceedings | 2015
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