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Calculators/Fluid Mechanics

Normal Shock: Downstream State and Pressure Loss

Inputs

Example values are filled in. Review them for your calculation.

Upstream static absolute pressure (Pa)

Upstream static temperature (K)

Specific gas constant (J/(kg·K))

Constant heat-capacity ratio γ

Upstream Mach (1 = zero-strength limit)

Results

Your results will appear here after calculation, with units and steps to help you review them.

References

NASA Glenn: Normal Shock Wave EquationsSource accessed 2026-09-08

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Normal Shock: Downstream State and Pressure Loss | Engivault