Compressible Nozzle

1. Solves 1-D Compressible flow in Convergent Divergent Nozzle. 2. Get mode of operation- Check whether existing nozzle is Subsonic Nozzle, Normal Shock exist in Nozzle, Under-expanded or Over-expanded Nozzle, under specified operating conditions. Compute Thrust, Exit Velocity, Exit Temperature and Mass Flow rate.