Oblique Shock Calculations   This form calculates properties of air flow through an oblique shock wave. The required input is the Mach number of the upstream flow and the wedge angle. The gas is assumed to be ideal air.   Tabulated Values
Inputs Upstream Mach Number (M1)   Wedge Angle, (delta)(Degrees)	Results Downstream Mach Number (M2)   Oblique Wave Angle (theta)(Degrees)   Static pressure ratio (P2/P1)

(c) 2006 AMME, University of Sydney.