To simulate the incompressible turbulent flows,two models,known as the simplified and highly stable lattice Boltzmann method(SHSLBM)and large eddy simulation(LES)model,are employed in this paper.The SHSLBM was develop...To simulate the incompressible turbulent flows,two models,known as the simplified and highly stable lattice Boltzmann method(SHSLBM)and large eddy simulation(LES)model,are employed in this paper.The SHSLBM was developed for simulating incompressible viscous flows and showed great performance in numerical stability at high Reynolds numbers,which means that this model is capable of dealing with turbulent flows by adding the turbulence model.Therefore,the LES model is combined with SHSLBM.Inspired by the less amount of grids required for SHSLBM,a local grid refinement method is used at relatively high Reynolds numbers to improve computational efficiency.Several benchmark cases are simulated and the obtained numerical results are compared with the available results in literature,which show excellent agreement together with greater computational performance than other algorithms.展开更多
This paper presents a robust sharp-interface immersed boundary method for simulating inviscid compressible flows over stationary and moving bodies.The flow field is governed by Euler equations,which are solved by usin...This paper presents a robust sharp-interface immersed boundary method for simulating inviscid compressible flows over stationary and moving bodies.The flow field is governed by Euler equations,which are solved by using the open source library OpenFOAM.Discontinuities such as those introduced by shock waves are captured by using Kurganov and Tadmor divergence scheme.Wall-slip boundary conditions are enforced at the boundary of body through reconstructing flow variables at some ghost points.Their values are obtained indirectly by interpolating from their mirror points.A bilinear interpolation is employed to determine the variables at the mirror points from boundary conditions and flow conditions around the boundary.To validate the efficiency and accuracy of this method for simulation of high-speed inviscid compressible flows,four cases have been simulated as follows:supersonic flow over a 15°angle wedge,transonic flow past a stationary airfoil,a piston moving with supersonic velocity in a shock tube and a rigid circular cylinder lift-off from a flat surface triggered by a shock wave.Compared to the exact analytical solutions or the results in literature,good agreement can be achieved.展开更多
基金J.Wu acknowledges the support of the National Natural Science Foundation of China(Grant No.12072158)the Natural Science Foundation of Jiangsu Province(Grant No.BK20191271)+1 种基金the Research Fund of State Key Laboratory of Mechanics and Control of Mechanical Structures(Nanjing University of Aeronautics and Astronautics)(Grant No.MCMS-I-0120G02)This work is also supported by the Priority Academic Program Development of Jiangsu Higher Education Institutions(PAPD).
文摘To simulate the incompressible turbulent flows,two models,known as the simplified and highly stable lattice Boltzmann method(SHSLBM)and large eddy simulation(LES)model,are employed in this paper.The SHSLBM was developed for simulating incompressible viscous flows and showed great performance in numerical stability at high Reynolds numbers,which means that this model is capable of dealing with turbulent flows by adding the turbulence model.Therefore,the LES model is combined with SHSLBM.Inspired by the less amount of grids required for SHSLBM,a local grid refinement method is used at relatively high Reynolds numbers to improve computational efficiency.Several benchmark cases are simulated and the obtained numerical results are compared with the available results in literature,which show excellent agreement together with greater computational performance than other algorithms.
基金Natural Science Foundation of Jiangsu Province(Grant No.BK20191271)the National Numerical Wind Tunnel Project(Grant No.NNW2019ZT2-B28).
文摘This paper presents a robust sharp-interface immersed boundary method for simulating inviscid compressible flows over stationary and moving bodies.The flow field is governed by Euler equations,which are solved by using the open source library OpenFOAM.Discontinuities such as those introduced by shock waves are captured by using Kurganov and Tadmor divergence scheme.Wall-slip boundary conditions are enforced at the boundary of body through reconstructing flow variables at some ghost points.Their values are obtained indirectly by interpolating from their mirror points.A bilinear interpolation is employed to determine the variables at the mirror points from boundary conditions and flow conditions around the boundary.To validate the efficiency and accuracy of this method for simulation of high-speed inviscid compressible flows,four cases have been simulated as follows:supersonic flow over a 15°angle wedge,transonic flow past a stationary airfoil,a piston moving with supersonic velocity in a shock tube and a rigid circular cylinder lift-off from a flat surface triggered by a shock wave.Compared to the exact analytical solutions or the results in literature,good agreement can be achieved.
