Review of numerical simulation on complex separated flow of iced airfoil

被引：0
|
作者：
Zhao B. [1 ,2 ]
Zhang H. [3 ]
Li J. [1 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi’an
[2] Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China Ltd, Shanghai
[3] School of Aerospace Engineering, Tsinghua University, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 01期
基金：
中国国家自然科学基金;
关键词：
iced airfoil; Large Eddy Simulation (LES); RANS/LES; Reynolds Averaged Navier-Stokes (RANS); separated flow;
D O I：
10.7527/S1000-6893.2022.27211
中图分类号：
学科分类号：
摘要：
The complex separation flow caused by icing will lead to the deterioration of aerodynamic performance, especially stall behavior. The accurate prediction of aerodynamic performance and the thorough investigation of mechanism under icing condition depend on the precise solution of the separated flow field. With the improvement of computational fluid dynamics methods especially turbulence simulation, the numerical simulation can reflect the physical nature of separated flow as well as provide precise and complete results. In terms of the application of three typical turbulence simulation methods, Reynolds Averaged Navier-Stokes(RANS), Large Eddy Simulation(LES)and RANS/ LES, a comprehensive review of recent research progress in numerical simulation on the prediction of stall behavior and characterization of separated flow are presented. Furthermore, the summary and outlook of the development tendency are also proposed in the aspects of high-fidelity ice shapes, new type turbulence simulation methods, deep analysis of unsteady features and real time coupling analysis of separated flow. © 2023 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
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