An adaptive integration method for hybrid-dimensional simulations of aeroengine flight statuses by incorporating computational fluid dynamics models of turbomachinery subcomponents-Reference-Cited by-同舟云学术

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An adaptive integration method for hybrid-dimensional simulations of aeroengine flight statuses by incorporating computational fluid dynamics models of turbomachinery subcomponents

Published:2024-08-27 Issue:1 Volume:18 Page:
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Deng Weimin¹,Wang Xiting²,Xu Yibing³,Xu Haoyang³

Affiliation:

1. Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology, Shenzhen, People's Republic of China

2. Institute for Aero Engine, Tsinghua University, Beijing, People's Republic of China

3. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, People's Republic of China

Publisher

Informa UK Limited

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2024.2391447

Reference42 articles.

1. Performance estimation of multi-stage cooled axial flow turbines under choked conditions

2. Towards the Large-Eddy Simulation of a full engine: Integration of a 360 azimuthal degrees fan, compressor and combustion chamber. Part I: Methodology and initialisation

3. Fully Coupled Turbojet Engine Computational Fluid Dynamics Simulations and Cycle Analyses Along the Equilibrium Running Line

4. Steady-state CFD Simulations of a Small-scale Turbojet Engine from Idle to Cruise Conditions

5. Effects of pulsed endwall air injection on corner separation and vortical flow of a compressor cascade

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