MAE 264
Computational Aerodynamics
Course Description
Numerical methods for aerodynamics flow simulation in the transonic regime. Solutions of steady and unsteady potential and compressible boundary layer equations. Numerical schemes for mixed type equations and shock waves/numerical grid generation. Viscous/inviscid interaction and coupling procedures.
Course Notes
- 4 Units
- Lecture: 4 hours
- Prerequisites: Engineering 180 or consent of instructor
- Offered in alternate years