Numerical Calculation of Wind Tip Vortex Formation for Different Wingtip devices
In this study numerical calculations are conducted to understand implementation of different wingtip device for wingtip vortexes formation. Numerical methods are performed over NACA 0012 winglet at the varying Reynolds numbers from 0.5x106 to 1x106 with the angle of attack 10° and compared with othe...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2018-09-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/sogukpinar__vol_10_iss_3.pdf |