Receptivity of Boundary Layers under Pressure Gradient
Boundary-layer flow over bodies such as aircraft wings or turbine blades is characterized by a pressure gradient due to the curved surface of the body. The boundary layer may experience modal and non-modal instability, and the type of dominant instability depends on whether the body is swept with re...
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| Format: | Others |
| Language: | English |
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KTH, Stabilitet, Transition, Kontroll
2008
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-9379 http://nbn-resolving.de/urn:isbn:978-91-7415-155-8 |