Airfoil aerodynamics analysis by using viscous-inviscid direct analysis
The main objective of this research is to develop computer code for airfoil aerodynamics analysis. The flow assumed to be incompressible and pass through a streamline body at relatively high Reynolds number. As result the flow domain around the airfoil can be divided into two regions, namely the flo...
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| Format: | Thesis |
| Published: |
2011
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| Subjects: | |
| Online Access: | http://eprints.uthm.edu.my/2414/ http://eprints.uthm.edu.my/2414/1/Mohd_Faizal.pdf |
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