Ability to distinguish incompressible and compressible flows.

Ability to understand the wave propagation phenomenon in subsonic, sonic and supersonic flows.

ability to solve one dimensional compressible flow problems involving area change

Ability to analyze  converging nozzles, real nozzles and rocket engines

Ability to solve one dimensional compressible flow problems involving stationary, moving and reflected shock waves.

Ability to analyze  de Laval nozzles, wind tunnels, jet engine inlets, real diffusers, supersonic Pitot tubes and shock tubes.

Ability to solve one dimensional compressible flow problems with friction.

Ability to analyze adiabatic ducts, which are fed by converging and de Laval nozzles.

Ability to solve one dimensional isothermal flow problems.

Ability to solve one dimensional compressible flow problems with heat transfer.

Ability to solve two dimensional compressible flow problems involving oblique shock waves, Prandtl-Meyer expansion waves.

Ability to analyze  overexpansion and underexpansion flow regimes in de Laval nozzles, oblique shock diffusers and airfoils.