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.
Main Author: | Mihaela CALUDESCU |
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Format: | Article |
Language: | English |
Published: |
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 |
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