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3. (1.5 pts) Consider a Mach 2.8 supersonic flow over a compression corner with a deflection angle of 15. If the deflect
Posted: Mon May 02, 2022 3:34 pm
by answerhappygod
- 3 1 5 Pts Consider A Mach 2 8 Supersonic Flow Over A Compression Corner With A Deflection Angle Of 15 If The Deflect 1 (21.05 KiB) Viewed 32 times
3. (1.5 pts) Consider a Mach 2.8 supersonic flow over a compression corner with a deflection angle of 15. If the deflection angle is doubled to 30. what is the increase in shock strength? 4. (1.5 pts) Consider a compression corner with a deflection angle of 28. Calculate the shock strengths when M1 = 3 and when Mi is doubled to 6. Is the shock strength doubled?