A high-order fluid-structure interaction framework with application to shock-wave/turbulent boundary-layer interaction over an elastic panel

被引:7
作者
Gao, Min [1 ]
Appel, Daniel [1 ]
Beck, Andrea [1 ]
Munz, Claus-Dieter [1 ]
机构
[1] Univ Stuttgart, Inst Aerodynam & Gas Dynam, Pfaffenwaldring 21, D-70569 Stuttgart, Germany
关键词
Fluid-structure interaction; Discontinuous Galerkin method; Shock capturing; Legendre spectral finite element methods; Implicit large eddy simulation; Shock-wave; turbulent boundary-layer; interaction; LARGE-EDDY SIMULATION; ELEMENT-METHOD; FINITE-VOLUME; CONSERVATION; ALGORITHMS; TURBULENCE; SOLVERS;
D O I
10.1016/j.jfluidstructs.2023.103950
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Within this work, a loosely-coupled high-order fluid-structure interaction (FSI) framework is developed in order to investigate the influence of an elastic panel response on shock-wave/turbulent boundary-layer interaction (SWTBLI). Since high-order methods are expected to determine the future of high-fidelity numerical simulations, they are employed in the construction of both fluid and structure solvers. Specifically, a split form arbitrary Lagrangian-Eulerian discontinuous Galerkin spectral element method is employed in the fluid solver and a Legendre spectral finite element method in the structure solver. Shock capturing by an improved adaptive filter method, which confines the filtering effect to the vicinity of shocks, is found to be well-behaved in accuracy, efficiency and flexibility.After being validated by two benchmark FSI problems, the developed FSI framework is applied to simulate SWTBLI over an elastic panel. A comparison with a previous simulation of SWTBLI over a rigid panel reveals that: (1) A larger amplitude of the pressure variation, observed on the elastic panel surface, implies a larger threat to the structural integrity; (2) The shock-induced separation flow over the elastic panel changes both in size and shape, leading to a different skin-friction coefficient distribution; (3) A new low-frequency flow unsteadiness of the same magnitude as the elastic panel vibration is detected, which may affect the flow dynamics inside the turbulent boundary layer.& COPY; 2023 Elsevier Ltd. All rights reserved.
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页数:30
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