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https://play.google.com/store/apps/d...ozzleflowfinal

1. Compressible flow in Convergent Divergent Nozzle2. Get mode of operation under specified operating conditions- Whether nozzle is Subsonic Nozzle, Normal Shock exist in Nozzle, location of Shock, Under-expanded or Over-expanded Nozzle. Compute Thrust, Exit Velocity, Exit Temperature and Mass Flow rate.
3. Optimization of Nozzle - Optimize Nozzle keeping fixed Area ration or Pressure ratio. Find...

https://play.google.com/store/apps/d...odynamicstools

The app is handy tool for Aerodynamic Engineers and Academicians. It contains Isentropic Relations, Normal Shock Relations, Oblique-Shock (Theta-Beta-Mach) Relations, Prandtl-Meyer Expansion wave Relations, Pitot Tube- Velocity computations, Y Plus or Y+ calculations.

1. Isentropic Relations - If any one of the variable from M, Po/P, To/T, Rho/Rh or A/A* is known and used as input, the remaining...