MAE 342 - Computational Methods in Aerospace Engineering

Introduces solid modeling software with applications to aircraft and spacecraft; solutions of the flow over aerodynamically shaped bodies using panel method codes and Navier Stokes codes; computation and analysis of aerodynamic quantities, such as lift, drag, and moments; and numerical methods for analyzing dynamics of spacecraft. (SI)

Prerequisites & Notes
Prerequisite: APMA 314 and MAE 321.

Credits: 3