EG 308

Gas Dynamics

This course provides students an opportunity to study the one-dimensional and quasi-one-dimensional compressible fluid flow with an emphasis on supersonic flow. The fundamental equations (continuity, momentum, and energy) that govern the characteristics of compressible flow are derived. The Mach number and various flow regimes are introduced. The phenomena and sources of normal shock waves, oblique shock waves, and Prandtl-Meyer expansion waves and their analysis techniques are presented. Other topics are: nozzles, diffusers, one-dimensional flow with heat addition (Rayleigh flow), one-dimensional flow with friction (Fanno flow), moving shock waves, shock tubes, and linearized supersonic theory.

Units: 3.0