Aerodynamic Optimization of a Single-Stage Transonic Axial Compressor with a Circumferential Feedback Channel-Reference-Cited by-同舟云学术

Aerodynamic Optimization of a Single-Stage Transonic Axial Compressor with a Circumferential Feedback Channel

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Dinh Cong-Truong¹^ORCID,Vuong Tien-Dung²,Kim Kwang-Yong³

Affiliation:

1. Dept. of Aerospace Engineering, Hanoi Univ. of Science and Technology, 1, Dai Co Viet Rd., Hai Ba Trung District, Hanoi 11615, Vietnam (corresponding author). ORCID: .

2. Master’s Student, Dept. of Mechanical Engineering, Inha Univ., 100, Inha-Ro, Michuhol-Gu, Incheon 22212, Republic of Korea.

3. Professor, Dept. of Mechanical Engineering, Inha Univ., 100, Inha-Ro, Michuhol-Gu, Incheon 22212, Republic of Korea.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4056

Reference44 articles.

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5. Chen H. X. Huang and S. Fu. 2006. “CFD investigation on stall mechanisms and casing treatment of a transonic compressor.” In Vol. 6 of Proc. Collection of Technical Papers-AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conf. 4789–4798. Sacramento CA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4799.