Influence on tip leakage flow in a compressor cascade with plasma actuation

Influence on tip leakage flow in a compressor cascade with plasma actuation

As one of the key components of aero engines, compressor is required to endure higher pressure,  possess  higher  efficiency  and  wider  operating  range. Intensive studies have been made on tip leakage flow and researchers find that by reasonably organizing tip leakage flow, aero engines are  more...

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Bibliographic Details
Main Author: Wang, Haotian
Format: Others
Language:English
Published: KTH, Skolan för industriell teknik och management (ITM) 2019
Subjects:
Flow control
DBD Plasma actuation
phenomenological model
numerical simulation
tip leakage flow
compressor cascade.
Flödesreglering
DBD Plasma‐aktuator
numerisk simulering
toppspelsflöde
kompressor kaskad.
Engineering and Technology
Teknik och teknologier
Online Access:http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264269

Internet

http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264269

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