Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap
Steady state, two-dimensional computational investigations performed on NACA 0012 airfoil to analyze the effect of variation in Reynolds number on the aerodynamics of the airfoil without and with a Gurney flap of height of 3% chord are presented in this paper. RANS based one-equation Spalart-Allmara...
में बचाया:
| मुख्य लेखकों: | , , |
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| स्वरूप: | Artigo |
| भाषा: | Inglês |
| प्रकाशित: |
Wiley
2015-01-01
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| श्रृंखला: | International Journal of Rotating Machinery |
| ऑनलाइन पहुंच: | http://dx.doi.org/10.1155/2015/628632 |
| टैग: |
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