Aeroacoustic Investigation of a Single Airfoil Tip Leakage Flow
نویسندگان
چکیده
منابع مشابه
Numerical Investigation for the Impact of Single Groove on the Stall Margin Improvement and the Unsteadiness of Tip Leakage Flow in a Counter-Rotating Axial Flow Compressor
A low-speed counter-rotating axial flow compressor (CRAC) with single circumferential grooved casing treatment (CT) was investigated numerically. Both steady and time-accurate numerical calculations were performed to study the effects of the single grooved CTs over the rear rotor on the stability enhancement and the unsteadiness of tip leakage flow (TLF) in the CRAC. Parametric studies indicate...
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ژورنال
عنوان ژورنال: International Journal of Aeroacoustics
سال: 2010
ISSN: 1475-472X,2048-4003
DOI: 10.1260/1475-472x.9.3.253