LAMINAR STABILITY ANALYSIS IN BOUNDARY LAYER FLOW
This study presents a numerical study concerning the flow control by suction and injection. The case study is over a symmetrical airfoil with suction and injection slots. The angle of attack is 3 degree with the Mach number 0.12.
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2009-09-01
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| Series: | INCAS Bulletin |
| Online Access: | http://bulletin.incas.ro/files/mihaela_caludescu_v1no1_full.pdf |
| Summary: | This study presents a numerical study concerning the flow control by suction and injection. The case study is over a symmetrical airfoil with suction and injection slots. The angle of attack is 3 degree with the Mach number 0.12. |
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| ISSN: | 2066-8201 2247-4528 |