多维迎风方法在非结构/混合网格热流计算中的应用研究  

Application of multi-dimensional upwind scheme in hypersonic aeroheating predictions on unstructured/hybrid grids

作　　者：万云博 马戎[1] 王年华[1] 张来平[1,2] 桂业伟[1] WAN Yun-bo;MA Rong;WANG Nian-hua;ZHANG Lai-ping;GUI Ye-wei(Computational Aerodynamics Institute,China Aerodynamic Research and Development Center, Mianyang 621000,China;China State Key Laboratory of Aerodynamics,China Aerodynamic Research and Development Center, Mianyang 621000,China)

机构地区：[1]中国空气动力研究与发展中心计算空气动力研究所,绵阳621000 [2]中国空气动力研究与发展中心空气动力学国家重点实验室,绵阳621000

出　　处：《计算力学学报》2019年第1期35-42,共8页Chinese Journal of Computational Mechanics

基　　金：国家重点研发计划(2016YB0200701);国家自然科学基金(11532016;91530325)资助项目

摘　　要：非结构/混合网格具有极强的几何灵活性,在复杂外形飞行器的气动力特性数值模拟中已得到广泛应用,但目前还难以准确地预测气动热环境。本文从非结构/混合网格热流计算的三个需求出发,选取了多维迎风方法,并与其他方法进行了对比研究。以二维圆柱高超声速绕流这一Benchmark典型问题为例,对比研究了多维迎风方法和几种广泛使用的无粘通量格式(Roe格式、Van Leer格式和AUSMDV格式)对混合网格热流计算精度的影响。结果表明,多维迎风方法在热流计算精度、鲁棒性以及收敛性方面表现良好。最后,将多维迎风方法应用于常规混合网格上的圆柱和钝双锥绕流问题,均得到了较好的热流计算结果,为非结构/混合网格热流计算在复杂高超飞行器中的应用奠定了基础。The unstructured/hybrid grid has a strong geometric flexibility and is widely used in the numerical simulation of aerodynamic characteristics of complex vehicles.However,it is hard to predict the aerothermodynamic environment accurately.Based on the three requirements of hypersonic aeroheating on unstructured/hybrid grid,a multi-dimensional upwind method is selected and studied intensively in this paper.The multi-dimensional upwind scheme and several widely used inviscid flux schemes(Roe,Van Leer and AUSMDV schemes)are compared based on the typical test case of hypersonic flow over a two-dimensional cylinder.The numerical results show that the multidimensional upwind method has a superior performance in terms of accuracy,robustness and convergence.Finally,the multidimensional upwind method is applied to predict the heat flux over a cylinder and a biconic configuration on the general hybrid grids.The numerical results of the heat flux are satisfactory,which demonstrates the capability for accurate aeroheating prediction over complex hypersonic vehicles on unstructured/hybrid grids.

关 键 词：非结构网格 混合网格 气动热环境 多维迎风方法 无粘通量格式 

分 类 号：O354.4[理学—流体力学] V211.3[理学—力学]