Isentropic Flow Calculator 2.0

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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