Lectures related to Supersonic aircraft

Covers isentropic flows, Mach waves, and their interaction in supersonic flows.

Covers relationships in oblique shock waves for perfect gases and their resolution procedures.

Explores conservation laws and Mach number effects in 1D flows.

Explores the performance advantages of convergent-divergent nozzles in supersonic applications.

Explores lift and drag forces, supersonic flow, and wave drag in Prandtl-Meyer flows.