Project Details
Description
An integrated acoustic boundary element method for unstructured mesh large eddy simulations in low Mach number
| Status | Finished |
|---|---|
| Effective start/end date | 2/1/14 → 1/31/15 |
Funding
- Stanford University
Fingerprint
Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.