Compressible Aerodynamics Calculator (1.1.1)

[Waverider]

This programs calculates Isentropic Flow Relations, Normal Shock Relations, Oblique Shock Relations, Prandtl–Meyer expansion, Fanno Flow and Rayleigh Flow for perfect gas.



HP Prime version by Bruno F Porto (me), Professor Henry T. Nagamatsu Laboratory of Aerothermodynamic and Hypersonics from the Institute for Advanced Studies, Brazil.

Based on the Javascript by William J. Devenport (and modified by Adam Ford to include Fanno Flow and Rayleigh Flow 7th February 2008), Department of Aerospace and Ocean Engineering, Virginia Tech.
http://www.dept.aoe.vt.edu/~devenpor/aoe3114/calc.html

Updates from 1.0 to 1.1: Added the Prandtl–Meyer expansion component!
Updates from 1.1 to 1.1.1: Corrected some minor local variables problems and the p0p0 (sub) upper limit at the Rayleigh Flow

I will soon update to add the Conical Shock Relations