Experimental study of corner separation and unsteady characteristics in linear compressor cascades with and without sweeping jet actuator-Reference-Cited by-同舟云学术

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Experimental study of corner separation and unsteady characteristics in linear compressor cascades with and without sweeping jet actuator

Published:2024-06 Issue: Volume: Page:
ISSN:2212-540X
Container-title:Propulsion and Power Research
language:en
Short-container-title:Propulsion and Power Research

Author:

Chen S.W.,Li W.H.,Xu C.,Meng Q.H.

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference45 articles.

1. A criterion for axial compressor hub-corner stall;Lei;ASME Journal of Turbomachinery,2008

2. Flow control on bowed compressor cascades using vortex generator jet at different incidences;Li;J. Aero. Eng.,2017

3. The effect of the pressure distribution in a three-dimensional flow field of a cascade on the type of curved blade;Wang,1994

4. The use of sweep and dihedral in multistage axial flow compressor blading — Part I: university research and methods development;Gallimore;ASME Journal of Turbomachinery,2002

5. Design Methodology for Spluttered Axial Compressor Rotors;Tzuoo,1990

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