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.