Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
This thesis evaluates the mechanism for inducing leading edge vortex using synthetic jet utilising ansys fluent on an airfoil due to aerodynamic in the transitional Reynolds number regime. Two-dimensional simulations based on the concept of fluid-structure interaction at low-to-moderate Reynold’s nu...
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| Format: | Monograph |
| Language: | English |
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Universiti Sains Malaysia
2021
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| Online Access: | http://eprints.usm.my/54539/1/Evaluation%20Of%20The%20Mechanisms%20For%20Inducing%20Leading%20Edge%20Vortex%20Using%20Ansys%20Fluent.pdf http://eprints.usm.my/54539/ |
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