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Publishing Language: Chinese

Evolution of compressor aerodynamic design methods

Taiqiu LIU1,2( )Lucheng JI1
Institute for Aero Engine, Tsinghua University, Beijing 100084, China
Aerospace Power System Safety Research Center, AECC Shenyang Engine Research Institute, Shenyang 110015, China
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Abstract

As a core component of aero-engines, the continuous advancement of compressor aerodynamic design methods has long been a key driver for performance improvement. This paper reviews the technological evolution of these design methods over the past eight decades, systematically outlines the key characteristics of aerodynamic design development, and highlights the co-evolutionary relationship among innovations in design methodologies, breakthroughs in engine performance, and iterative advancements in computational technologies. Against the backdrop of exponential growth in computing power and algorithm efficiency, new compressor aerodynamic design approaches are emerging rapidly, accelerating the transition toward intelligent screening and multi-disciplinary coupling. Meanwhile, traditional low-dimensional empirical methods are being enhanced through intelligent algorithms that build general model libraries, enabling rapid evaluations within defined parameter ranges. In the context of the digital transformation of the aero-engine industry, the future compressor aerodynamic design system is expected to follow an integrated development path where empirical models, numerical simulations, and intelligent algorithms complement each other, achieving a co-evolutionary paradigm that combines innovative fusion with improved engineering efficiency.

CLC number: V231.1 Document code: A Article ID: 1000-6893(2026)12-132631-26

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
LIU T, JI L. Evolution of compressor aerodynamic design methods. Acta Aeronautica et Astronautica Sinica, 2026, 47(12). https://doi.org/10.7527/S1000-6893.2025.32631

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Received: 28 July 2025
Revised: 19 August 2025
Accepted: 04 December 2025
Published: 02 January 2026
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica