LAMINAR STABILITY ANALYSIS IN BOUNDARY LAYER FLOW
Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 1
Abstract
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.
Authors and Affiliations
CALUDESCU Mihaela
Keywords
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- EP ID EP114928
- DOI 10.13111/2066-8201.2009.1.7
- Views 74
- Downloads 0
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