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 =

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
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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