Technical Papers
Jan 18, 2024

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

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

This study presents a design optimization of a circumferential feedback channel on the shroud casing between rotor trailing and leading edges to maximize the aerodynamic performance of a single-stage transonic axial compressor, NASA Stage 37, using three-dimensional Reynolds-averaged Navier–Stokes analysis (RANS) with the k-ε turbulence model. The location of the injection and bleeding ports, angles of injection, and bleeding were the most influential factors on the aerodynamic performance and were selected as the design variables. A hybrid genetic algorithm and particle swarm optimization algorithm coupled with three different surrogate models were utilized to maximize the peak adiabatic efficiency and stall margin of the transonic axial compressor. The optimization results for the circumferential feedback channel indicated that an increase in stall margin was achievable with a slightly reduced peak efficiency in comparison with that of the smooth casing.

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Data Availability Statement

All data, models, and code generated or used during the study appear in the published article.

Acknowledgments

This work is supported by the Vietnam National Foundation for Science and Technology Development under Grant No. 107.03-2018.20.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: May 28, 2021
Accepted: Sep 13, 2023
Published online: Jan 18, 2024
Published in print: May 1, 2024
Discussion open until: Jun 18, 2024

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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: https://orcid.org/0000-0001-5357-1534. Email: [email protected]
Tien-Dung Vuong [email protected]
Master’s Student, Dept. of Mechanical Engineering, Inha Univ., 100, Inha-Ro, Michuhol-Gu, Incheon 22212, Republic of Korea. Email: [email protected]
Kwang-Yong Kim, Ph.D. [email protected]
Professor, Dept. of Mechanical Engineering, Inha Univ., 100, Inha-Ro, Michuhol-Gu, Incheon 22212, Republic of Korea. Email: [email protected]

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