Stability Improvement of a High-Pressure Ratio Centrifugal Compressor by Flow Injection-Reference-Cited by-同舟云学术

Stability Improvement of a High-Pressure Ratio Centrifugal Compressor by Flow Injection

Published:2020-11 Issue:6 Volume:33 Page:04020072
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Wenchao¹,He Xiao¹,Wang Baotong²,Sun Zhenzhong³,Zheng Xinqian⁴

Affiliation:

1. Master Student, Turbomachinery Laboratory, State Key Laboratory of Automotive Safety and Energy, Tsinghua Univ., No. 30, Shuangqing St., Haidian District, Beijing 100084, China.

2. Associate Professor, Institute for Aero Engine, Tsinghua Univ., No. 30, Shuangqing St., Haidian District, Beijing 100084, China (corresponding author).

3. Assistant Professor, Institute for Aero Engine, Tsinghua Univ., No. 30, Shuangqing St., Haidian District, Beijing 100084, China.

4. Professor, Institute for Aero Engine, Tsinghua Univ., Shuangqing St., Haidian District, Beijing 100084, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001191

Reference23 articles.

1. Flow Control of Extreme Pressure Loads Associated with Flow Separation

2. Culley D. E. Braunscheidel and M. Bright. 2005. “Impulsive injection for compressor stator separation control.” In Proc. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit. New York: AIAA.

3. Active Flow Separation Control of a Stator Vane Using Embedded Injection in a Multistage Compressor Experiment

4. Active Suppression of Rotating Stall and Surge in Axial Compressors

5. Effect of endwall vortex generator jets on flow separation control in a linear compressor cascade

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