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Normal Shock Waves

- Characteristic Mach number
- Characteristic Mach Number behind shock
- Critical speed of sound from Prandtl relation
- Density ahead of normal shock using normal shock momentum equation
- Density behind normal shock for given upstream density and Mach number
- Density behind normal shock using normal shock momentum equation
- Density ratio across a normal shock
- Enthalpy ahead of normal shock from normal shock energy equation
- Enthalpy behind of normal shock from normal shock energy equation
- Entropy change across normal shock
- Mach Number behind the shock
- 19 More formulas!

Oblique Shock and Expansion Waves

- Component of Downstream Mach normal to oblique shock
- Component of downstream Mach number normal to oblique shock for given normal upstream Mach number
- Component of Upstream Mach normal to oblique shock
- Density behind oblique shock for given upstream density and normal upstream Mach number
- Density ratio across the oblique shock
- Flow deflection angle
- Flow deflection angle in terms of Prandtl Meyer function
- Forward Mach angle of expansion fan
- Prandtl Meyer function
- Prandtl Meyer function at upstream Mach number
- Pressure behind expansion fan
- 9 More formulas!

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