Study made to explore use of interference pressures to reduce afterbody drag of missile or airplane and effect of important variables such as jet-exit pressure ratio, nacelle position relative to afterbody, afterbody shape, and angle of attack; results show trends in axial-force variation with above variables near conditions for maximum jet-afterbody interference.
Axial-force reduction by interference between jet and neighboring afterbody
NASA -- Tech Note
1960
95 pages
Report
English
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