Abstract
The optimal disturbances/streamwise vortices associated with the transient growth mechanism was performed for boundary layers in the presence of a streamwise pressure gradient. The theory provided the optimal spacing of the control elements in the spanwise direction and their placement in the streamwise direction.
| Original language | English (US) |
|---|---|
| Pages (from-to) | 2297-2300 |
| Number of pages | 4 |
| Journal | AIAA journal |
| Volume | 41 |
| Issue number | 11 |
| DOIs | |
| State | Published - Nov 2003 |
ASJC Scopus subject areas
- Aerospace Engineering