Aerodynamic Optimization Based on the Euler and Navier-Stokes Equations using Unstructured Grids
The overall problem area addressed is that of efficient aerodynamic shape design through the use of computational fluid dynamics (CFD). A method is presented for performing optimization including modal inverse design and lift-constrained drag minimization -- based on the 2D and 3D Euler equations a...
| Main Author: | |
|---|---|
| Format: | Technical Report |
| Language: | en_US |
| Published: |
Aerospace Computational Design Laboratory, Dept. of Aeronautics & Astronautics, Massachusetts Institute of Technology
2010
|
| Online Access: | http://hdl.handle.net/1721.1/57602 |