【實用工具app】Compressible Flow|最夯免費app

Compressible Flows Equations:

1) Isentropic relationships

2) Normal Shock Calculator for aerodynamics compressible flows

3) Gas properties, more will be added

P0=stagnation pressure, T0=stagnation temperature

Equations:

P0=P*(1+0.5(gamma-1)Mach^2)^(gamma)/(gamma-1)

T0=T*(1+0.5(gamma-1)Mach^2)

For engineering students and/or aerospace engineers; let me know how I can improve this app

The Heat Capacity ratio of the gas can be changed and few references values can be chosen

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

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