Experimental and Numerical Investigations of Inlet Circumferential Fluctuations in Swept Compressor Cascades-Reference-Cited by-同舟云学术

Experimental and Numerical Investigations of Inlet Circumferential Fluctuations in Swept Compressor Cascades

Published:2023-09 Issue:5 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Jiancheng¹^ORCID,Jin Donghai²,Li Zefeng³,Wen Lei⁴,Zhang Jian⁵,Liu Xiaoheng⁶,Gui Xingmin⁷

Affiliation:

1. Ph.D. Candidate, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China. ORCID: .

2. Associate Professor, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China; Associate Professor, Jiangxi Research Institute, Beihang Univ., Jiangxi 330096, China.

3. Engineer, Dept. of Turbine Research, Aero Engine Corporation of China (AECC) Hunan Aviation Powerplant Research Institute, Zhuzhou 412002, China.

4. Engineer, Dept. of Product Design, Shanghai Electric Gas Turbine Co., Ltd., Jiangchuan Rd., Shanghai 200240, China.

5. Research Fellow, Dept. of Turbine Research, Aero Engine Corporation of China Sichuan Gas Turbine Establishment, Chengdu 610500, China.

6. Postdocdoral Student, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China; Postdocdoral Student, Jiangxi Research Institute, Beihang Univ., Jiangxi 330096, China (corresponding author).

7. Professor, School of Energy and Power Engineering, Beihang Univ., Beijing 100191, China; Professor, Jiangxi Research Institute, Beihang Univ., Jiangxi 330096, 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-4777

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5. The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part I: University Research and Methods Development