Experimental Investigation of Shock Wave-Boundary Layer Interaction on a Generic Oscillating Bump
The presented research investigates the effects of shock wave boundary layer interaction on the unsteady pressure response of the surface of an oscillating structure. A simplified structure, a 2D prismatic bump, located in a straight channel is used to better understand the bending flutter phenomeno...
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| Format: | Others |
| Language: | English |
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KTH, Kraft- och värmeteknologi
2014
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-156059 |