Oblique Shock Calculator

Oblique Shock Calculator

Must be > 1.0 for supersonic flow.

10°45°90°

Shock Properties

Deflection Angle (θ)0.00°
Downstream Mach (M₂)0.000
Pressure Ratio (P₂/P₁)0.000

Understanding Oblique Shocks

Oblique shocks occur when supersonic flow is turned into itself. The shock angle (β) is the angle between the shock wave and the upstream flow direction, while the deflection angle (θ) is how much the flow turns.

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