Consider the flow over a 22.2° half-angle wedge. If M1 = 2.5, p1 = 1atm, and T1 = 300 K, calculate the wave angle and p2, T2, and M2.

Question

Robert · Accepted Answer

Given Data: 
Half Wedge Angle A = 22.2 deg. 
Mach Number M1 = 2.5 
Input Pressure P1 = 1 bar = 101325 Pa 
Temperature Before Shock T1 = 300 K
Using Oblique Shock Tables from , 
http://www-
mdp.eng.cam.ac.uk/web/library/enginfo/aerothermal_dvd_only/aero/oblique/obtable.html 
for M=2.5, A=22.

Consider the flow over a 22.2° half-angle wedge. If M1 = 2.5, p1 = 1atm, and T1 = 300 K, calculate the wave angle and p2, T2, and M2.

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