laminar stability analysis in boundary layer flow
Clicks: 170
ID: 206288
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.
| Reference Key |
caludescu2009incaslaminar
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|---|---|
| Authors | ;Mihaela CALUDESCU |
| Journal | biotechnology letters |
| Year | 2009 |
| DOI |
10.13111/2066-8201.2009.1.1.7
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| URL | |
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