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) |
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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