首页|Enhanced quasi-three-dimensional transient simulation technique incorporating component volume effects for aero engine

Enhanced quasi-three-dimensional transient simulation technique incorporating component volume effects for aero engine

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Current transient analysis predominantly relies on zero-dimensional/one-dimensional tools,proficient at capturing aerothermodynamic variations across critical engine stations but insuf-ficient for analyzing the internal flow field evolution during transients.Addressing this gap,the study presents an enhanced quasi-three dimensional(quasi-3D)transient simulation technique that integrates component volume effects,offering a significant leap from the preceding quasi-3D tran-sient simulation method based on quasi-steady assumption.By embedding the component volume effects on density,momentum,and energy within the physical temporal dimension of the Navier-Stokes equations,the refined quasi-3D transient model achieves a closer representation of physical phenomena.Validation against a single-shaft turbofan engine's experimental data confirms the model's accuracy.Average errors for key performance indicators,including shaft speed,thrust,mass flow rate,and critical component exit temperature and pressure,remain below 0.41%,5.69%,2.55%,3.18%and 0.67%,respectively.Crucially,the model exposes a discernible temporal lag in the compressor outlet pressure and temperature response due to volume effects—previously unquantified in quasi-3D transient simulations.And further exploration of the meridional flow field emphasizes the consequential role of volumes in transient flow field evolution.Incorporating vol-ume effects within quasi-3D transient simulations enhances engine modeling and is pivotal for pre-cise transient analysis in engine design and optimization.

EnginesTransient simulationQuasi-3D modelingComponent volume effectsFlow field evolutionTransient performance analysis

Yuchen DAI、Manxiang SONG、Donghai JIN、Xingmin GUI

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Aeroengine Simulation Research Center,School of Energy and Power Engineering,Beihang University,Beijing 100191,China

Jiangxi Research Institute of Beihang University,Nanchang 330096,China

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(12)