MAE 212Introductory Compressible Flow
Equations of motion for compressible fluids; one-dimensional gas dynamics and wave motion, waves in supersonic flow, including oblique shock waves; flow in ducts, nozzles, and wind tunnels; methods of characteristics.
Prerequisites
From the catalog: “nongraduate students may enroll with consent of instructor.”
Where it sits in degree plans
Required in (1)
- AeroEng w/Spec Aerothermodynam
Courses that list MAE 212 as a prerequisite (1)
- MAE 213 Mechanics of Propulsion