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A supersonic wedge moves through a stationary atmosphere(u=0) at M=4. FIND THE ABSOLUTE flow direction behind the oblique shock with respected to the line of
A supersonic wedge moves through a stationary atmosphere(u=0) at M=4. FIND THE ABSOLUTE flow direction behind the oblique shock with respected to the line of flight. The deflection angle is 17.8. Atmosphere is a calorically perfect gas gamma=1.4, R=287, P=1atm. Answer: 59.95 degree to the line of flight. In detail
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Physics Principles With Applications ()
Authors: Douglas C. Giancoli Page
5th Edition
0136119719, 9780136119715
