The Influence of Steady Air Jet on the Trailing-Edge Shock Loss in a Supersonic Compressor Cascade

To effectively reduce shock wave loss at the trailing edge of a supersonic cascade under high back-pressure, a shock wave control method based on air jets is proposed. The air jet was arranged on the pressure side of the blade in the upstream of the trailing-edge shock. The flow control mechanism an...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Yinxin Zhu, Zhenbing Luo, Wenqiang Peng, Qiang Liu, Yan Zhou, Wei Xie, Pan Cheng, Zhengxue Ma, Xuzhen Xie
Format:	Article
Language:	English
Published:	MDPI AG 2022-11-01
Subjects:	supersonic compressor cascade trailing-edge shock air jet shock control total pressure loss
Online Access:	https://www.mdpi.com/2226-4310/9/11/713