A Zero-Dimensional Physics–Based Model to Guide Supersonic Rotor Design of a Counterrotating Compressor-Reference-Cited by-同舟云学术

A Zero-Dimensional Physics–Based Model to Guide Supersonic Rotor Design of a Counterrotating Compressor

Published:2023-11 Issue:6 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhao Ben¹,Zhou Xiaoxiao²,Liu Yongzhen³,Cui Weiwei⁴,Ma Fanhua⁵

Affiliation:

1. Professor, School of Energy Power and Mechanical Engineering, North China Electric Power Univ., No. 2 North Agricultural Rd., Changping District, Beijing 102206, China.

2. Ph.D. Student, Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beisihuan West Rd. No. 11, Haidian, Beijing 100190, China.

3. Assistant Researcher, School of Vehicle and Mobility, Tsinghua Univ., Shuangqing Rd. No. 30, Haidian, Beijing 100084, China (corresponding author).

4. Associate Professor, College of Civil Engineering and Architecture, Shandong Univ. of Science and Technology, Qianwangang Rd. No. 579, Huangdao, Qingdao 266590, China.

5. Associate Professor, School of Vehicle and Mobility, Tsinghua Univ., Shuangqing Rd. No. 30, Haidian, Beijing 100084, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4685

Reference29 articles.

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2. Shock/Boundary-Layer/Tip-Clearance Interaction in a Transonic Rotor Blade

3. Cai R. W. Wu and G. Fang. 1990. “Basic analysis of counter-rotating turbines.” In Vol. 79047 of Proc. Turbo Expo: Power for Land Sea and Air. New York: ASME. https://doi.org/10.1115/90-GT-108.

4. A new method for predicting performance of axial-flow compressor;Cai Y.-H.;Int. J. Turbo Jet Engines,1995

5. An Analytical Model of Axial Compressor Off-Design Performance