Compressible fluid equations: Isentropic Flow Calculator For engineering students and/or aerospace engineers
P0=stagnation pressure, T0=stagnation temperatureEquations:P0=P*(1+0.5(gamma-1)Mach^2)^(gamma)/(gamma-1)T0=T*(1+0.5(gamma-1)Mach^2)
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
VERSION HISTORY
- Version 2.0 posted on 2012-07-11
Program Details
- Category: System Utilities > System Maintenance
- Publisher: aero-calculator
- License: Free
- Price: N/A
- Version: 2.0
- Platform: android