Normal Shock Wave Calculations
This form calculates properties of air flow through a normal shock wave.The required input is the Mach number of the upstream flow. The gas is initially assumed to be ideal, non-reacting .
 | Inputs | Results |
This form calculates properties of air flow through a normal shock wave.The required input is the Mach number of the upstream flow. The gas is initially assumed to be ideal, non-reacting .
| | Inputs | Results |