A tip clearance prediction model for multistage rotors and stators in aero-engines-Reference-Cited by-同舟云学术

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A tip clearance prediction model for multistage rotors and stators in aero-engines

Published:2021-02 Issue:2 Volume:34 Page:343-357
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

SUN Huibin,WANG Jing,CHEN Kai,XIA Huateng,FENG Xin,CHANG Zhiyong

Funder

National Defense Basic Scientific Research Program of China

Foundation of Equipment Pre-research Area

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference33 articles.

1. Effect of tip clearance on the prediction of nonsynchronous vibrations in axial compressors;Drolet;J Turbomach,2013

2. Effect of nonuniform tip clearance on the performance of transonic axial compressors;Li;J Propul Power,2018

3. Prediction of the nonuniform tip clearance effect on the axial compressor flow field;Kang;J Fluid Eng-T ASME,2010

4. Nonuniform flow in a compressor due to asymmetric tip clearance;Song;J Turbomach,2000

5. Performance estimation method for nonuniform tip clearance cases;Chen;J Propul Power,2018

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2. Recent progress in precision measurement and assembly optimization methods of the aero-engine multistage rotor: A comprehensive review;Measurement;2024-08

3. Assembly accuracy analysis and phase optimization of aero-engine multistage rotors considering surface morphology and non-uniform contact deformation;Precision Engineering;2024-06

4. Prediction and Analysis of Transient Turbine Tip Clearance Using Long Short-Term Memory Neural Network;Journal of Engineering for Gas Turbines and Power;2024-05-13

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