Normal Shock Tables

Compressible flow equations
Normal Shock Calculator for aerodynamics compressible flows

For engineering students and/or aerospace engineers

The Heat Capacity ratio of the gas can be changed and few references values are shown in the app

More data can be found on http://en.wikipedia.org/wiki/Heat_capacity_ratio

Disclaimer:
I have checked the equations but it is always possible to have a bug; double check the results

fonts used in the icon Crimson Text: http://aldusleaf.org/index.php