Flap Gap Oscillatory Blowing on 2D and 2.5D Wing
Here we present preliminary results obtained in developing an active flow control system for highlift systems at advanced TRL level. The work is based on theoretical and experimental workperformed in AVERT EU FP6 project where the oscillatory flap gap blowing system was designedand tested on a INCAS...
| Main Author: | |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-12-01
|
| Series: | INCAS Bulletin |
| Online Access: | http://bulletin.incas.ro/files/catalin_nae_v1no2_2_full.pdf |