Study of tip clearance flows
The tip leakage vortex is responsible for the generation of stagnation pressure losses inside the compressor along with the outbreak of rotating stall and surge. The current paper analytically proved that a part of the losses is proportional to the vortex circulation squared. The evolution of this c...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2018
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-244423 |