A two-dimensional hypersonic vehicle defined in the figure below is flying with an angle of attack 10° and Mach number o
Posted: Sun May 15, 2022 11:14 pm
A two-dimensional hypersonic vehicle defined in the figure below is flying with an angle of attack 10° and Mach number of 8. Assume that the specific heat ratio of air is y=1.4. a=10° -% R V.. R2 L L2 L L =0.6m, L2 =1.2m, R, =0.3m, R2 =0.5m By using the shock-expansion method, calculate the lift coefficient of the vehicle (you can assume a free-stream pressure in the base region).