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
免費玩Compressible Flow APP玩免費
免費玩Compressible Flow App
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| 熱門國家 | 系統支援 | 版本 | 費用 | APP評分 | 上架日期 | 更新日期 |
|---|---|---|---|---|---|---|
| 未知 | Android Google Play | 2.0 App下載 | 免費 | 1970-01-01 | 2015-03-11 |
