The angle of the oblique shock wave= Mach number downstream the shock wave = Stagnation pressure downstream the shock wave =
The angle of the oblique shock wave= Mach number downstream the shock wave = Stagnation pressure downstream the shock wave =
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The angle of the oblique shock wave=
Mach number downstream the shock wave =
Stagnation pressure downstream the shock wave =
The speed of air along the turned wall (V2) =
The pressure downstream the oblique shock wave =
From the followings, select the turning angle that leads to detach the oblique shock wave from the corner.
The dynamic temperature of air along the turned wall =

Transcribed Image Text:The speed of a uniform air flow flowing
over a concave corner is 1038 m/s with a temperature
and pressure of 298 K and 100 kPa, respectively. The
turning angle of the corner e = 10°. Answer the
followings:
Oblique Shock
wave
M1
T1
P1
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