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LAMINAR STABILITY ANALYSIS IN BOUNDARY LAYER FLOW

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Author(s): Mihaela CALUDESCU

Journal: INCAS Bulletin
ISSN 2066-8201

Volume: 1;
Issue: 1;
Start page: 33;
Date: 2009;
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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.
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