AERODYNAMIC PERFORMANCES OF A SINGLE-STAGE TRANSONIC AXIAL COMPRESSOR USING AN INCLINED CASING GROOVE-Reference-Cited by-同舟云学术

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AERODYNAMIC PERFORMANCES OF A SINGLE-STAGE TRANSONIC AXIAL COMPRESSOR USING AN INCLINED CASING GROOVE

Published:2022-05-03 Issue: Volume: Page:1-10
ISSN:1448-4846
Container-title:Australian Journal of Mechanical Engineering
language:en
Short-container-title:Australian Journal of Mechanical Engineering

Author:

Nguyen Anh-Tuan¹,Vo Huynh-Duc²,Dinh Cong-Truong²,Chu Hoang-Quan³

Affiliation:

1. Department of Mechatronics, Hanoi University of Science and Technology, Hanoi, Vietnam

2. Department of Aeronautical and Space Engineering, Hanoi University of Science and Technology, Hanoi, Vietnam

3. Department of Reaction Engine, Le Quy Don Technical University, Hanoi, Vietnam

Funder

Hanoi University of Science and Technology

Publisher

Informa UK Limited

Subject

Mechanical Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/14484846.2022.2070100

Reference24 articles.

1. Performance enhancement in transonic axial compressors using blade tip injection coupled with casing treatment

2. Parametric Study of Tip Clearance—Casing Treatment on Performance and Stability of a Transonic Axial Compressor

3. Aerodynamic and structural performances of a single-stage transonic axial compressor with blade fillet radius

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effects of Axisymmetric Rotor Injection on the Aerodynamic Performances of a Single-Stage Transonic Axial Compressor;Lecture Notes in Mechanical Engineering;2024

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