航空发动机燃烧室多物理场的代理求解与模型封闭研究综述

Translated title of the contribution: A review of surrogate solving and model closure for multiphysics fields in aero-engine combustors
  • Chi Zhang
  • , Shihong Zhang
  • , Bosen Wang*
  • , Yuzhen Lin
  • , Minglong Zhao
  • , Shuhua Zhang
  • , Hongda Gao
  • , Shu Guo
  • *Corresponding author for this work

Research output: Contribution to journalReview articlepeer-review

Abstract

As one of the critical parts of an aero-engine, the effective organization of complex turbulent combustion within the combustor is essential for enhancing the performance of the combustor, the aero-engine, and even the entire aircraft. To achieve high-fidelity analysis of this turbulent combustion process, methods such as experimental measurements, numerical simulations, and neural networks have been increasingly applied in the field of aero-engine combustion. Neural networks, which effectively integrate multi-fidelity data and physical information, introduce a data-centric fourth paradigm of scientific research, alongside the empirical, theoretical, and simulation-based paradigms. Consequently, neural networks hold the potential to assist traditional experimental measurements and numerical simulations in obtaining higher-fidelity combustion field data at a lower cost. This paper focuses on the challenges and bottlenecks in analyzing combustion reaction flows, introduces representative neural network methods with potential applications in this domain, and reviews the current status and future prospects of neural network applications in combustion and related fields.

Translated title of the contributionA review of surrogate solving and model closure for multiphysics fields in aero-engine combustors
Original languageChinese (Traditional)
Article number202410002
JournalTuijin Jishu/Journal of Propulsion Technology
Volume47
Issue number1
DOIs
StatePublished - 10 Jan 2026

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