Normal Shock: Downstream State and Pressure Loss

Name: ENGiVAULT API
Author: Luqman Ismat

Inputs

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

Enter inputs and click calculate to see the result.

References

Normal Shock: Downstream State and Pressure Loss | Engivault