Design and aerodynamic stability improvement study of a non-axisymmetric stator fan in a distorted insertion plate configuration-Reference-Cited by-同舟云学术

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Design and aerodynamic stability improvement study of a non-axisymmetric stator fan in a distorted insertion plate configuration

Published:2024-12 Issue: Volume:155 Page:109537
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Sun Peng^ORCID,Yu Junyang,Fu Wenguang,Zhang Tao,Wang Chunxue,Zhao Wei

Publisher

Elsevier BV

Reference47 articles.

1. Aeromechanical response of a distortion-tolerant boundary layer ingesting fan;Provenza;J. Eng. Gas Turbine Power,2019

2. Distortion-induced vibration in fan and compressor blading;Danforth;J. Aircr.,1975

3. Inlet flow distortion effects in aircraft gas turbine engine compression systems;Sivapragasam,2009

4. Experimental investigation of circumferential inlet distortion on partial surge type stall inception in a transonic axial compressor;Yan;J. Propuls. Technol.,2023

5. D.X. Liu, P.L. Ye, J. Hu, Stability Design and Evaluation Technology of Aviation Gas Turbine Engine, Beijing: Aviation Industry Press2004.

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