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Numerical Study on Aerodynamic Performance of Hypersonic Vehicle with Aerospikes Read chapter Read first chapter

2022 | OriginalPaper | Chapter

Experimental Research on the Influence of the Bulk Swirl on the Compressor

Authors : Feng Lu-ning, Cheng Bang-qin, Wang Jia-le, Tao Ping, Wu Qiang

Published in: Aerospace Mechatronics and Control Technology

Publisher: Springer Nature Singapore

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Abstract

In order to explore the effect of the overall vortex flow distortion on the performance of the low-speed axial compressor, this paper carried out the compressor characteristic experiment under the overall vortex flow distortion generator based on the overall vortex flow distortion generator, and measured the performance of the swirl flow distortion generator. The generated swirl field obtains the pressure ratio and efficiency characteristics of the compressor under the conditions of uniform intake and swirl intake. The results show that the overall vortex flow distortion increases the pressure ratio of the compressor, reduces the efficiency of the compressor, and at the same time causes the stability margin of the compressor to decrease.

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Metadata
Title
Experimental Research on the Influence of the Bulk Swirl on the Compressor
Authors
Feng Lu-ning
Cheng Bang-qin
Wang Jia-le
Tao Ping
Wu Qiang
Copyright Year
2022
Publisher
Springer Nature Singapore
Book
Aerospace Mechatronics and Control Technology

Print ISBN: 978-981-16-6639-1

Electronic ISBN: 978-981-16-6640-7

Copyright Year: 2022

DOI
https://doi.org/10.1007/978-981-16-6640-7_11

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