Analysis and control of boundary layer transition on a NACA 0008 wing profile
The main aim of this thesis was to understand the mechanism behind the classical transition scenario inside the boundary layer over an airfoil and eventually attempting to control this transition utilizing passive devices for transition delay. The initial objective of analyzing the transition phenom...
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| Format: | Others |
| Language: | English |
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KTH, Mekanik
2018
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931 |