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)|
|Number of pages||4|
|Publication status||Published - Nov 2003|
ASJC Scopus subject areas
- Aerospace Engineering