1) Isentropic relationships
2) Normal Shock Calculator for aerodynamics compressible flows
3) Oblique Shock
4) 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
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
We do not host Compressible Flow Pro on our servers. We did not scan it for viruses, adware, spyware or other type of malware. This app is hosted by Google and passed their terms and conditions to be listed there. We recommend caution when installing it.
The Google Play link for Compressible Flow Pro is provided to you by apps112.com without any warranties, representations or guarantees of any kind, so access it at your own risk.
If you have questions regarding this particular app contact the publisher directly. For questions about the functionalities of apps112.com contact us.
|
| ||||
| Downloads: 8 | ||||
| Updated At: 2024-04-22 15:39:17 | ||||
| Publisher: aero-calculator | ||||
| Operating System: Android | ||||
| License Type: Free |