Oblique Shock Wave Calculations

This form calculates properties of gas flow through an oblique shock wave created by a small deflection. The required input is the Mach number of the upstream flow, ratio of specific heats of the gas and the wedge angle.
 
Input Parameters
Mach Number

Ratio of Specific Heats

Wedge Deflection Angle (Deg)


 
 
 
Wave Angle (deg) = 30.81
Downstream Mach Number = 1.9639
Pressure Ratio Across Shock Wave = 1.0577