You are here

- Home »
- Physics »
- Gas Dynamics

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 no. normal to oblique shock for given normal upstream Mach no.
- Component of Downstream Mach normal to oblique shock
- Component of Upstream Mach normal to oblique shock
- Density behind oblique shock for given upstream density & normal upstream Mach no.
- 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 no.
- Pressure behind expansion fan
- 9 More formulas!

Gas Dynamics calculators give you a list of online Gas Dynamics calculators. A tool perform calculations on the concepts and applications for Gas Dynamics calculations.

These calculators will be useful for everyone and save time with the complex procedure involved to obtain the calculation results. You can also download, share as well as print the list of Gas Dynamics calculators with all the formulas.