UZB 310E - Compressible Aerodynamics

Course Objectives

Two dimensional subsonic compressible steady and isentropic flows. Linear theory for subsonic and supersonic flows. Supersonic airfoils. Normal shocks. Oblique shocks. Expansion waves. Nozzles, diffusers and wind tunnels.

Course Description

Two dimensional subsonic compressible steady and isentropic flows. Linear theory for subsonic and supersonic flows. Supersonic airfoils. Normal shocks. Oblique shocks. Expansion waves. Nozzles, diffusers and wind tunnels.