Experiment investigation on the effect of inlet circumferential non-uniformity on the stall behaviours in a transonic axial compressor with axisymmetric stall precursor-Reference-Cited by-同舟云学术

Experiment investigation on the effect of inlet circumferential non-uniformity on the stall behaviours in a transonic axial compressor with axisymmetric stall precursor

Published:2022-09 Issue: Volume:128 Page:107781
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Pan Tianyu,Yan Jiandong^ORCID,Yan Zhaoqi,Sun Dakun,Li Qiushi

Publisher

Elsevier BV

Subject

Aerospace Engineering

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1. Impact of circumferential inlet distortion on different types of stall inceptions in a transonic compressor;Chinese Journal of Aeronautics;2024-07

2. A Methodology for Assessing Axial Compressor Stability with Inlet Temperature Ramp Distortion;Journal of Thermal Science;2024-04-01

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4. Partial tip air injection to extend the stall margin in an axial flow compressor with circumferential inlet distortion;Aerospace Science and Technology;2024-01

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