网格自适应策略在高升力构型计算中的应用  

Application of New Grid Adaptation Strategy on High Lift Configuration

作　　者：谭伟伟[1] 

机构地区：[1]中国航空计算技术研究所,陕西西安710068

出　　处：《航空计算技术》2010年第6期38-42,共5页Aeronautical Computing Technique

基　　金：总装预研基金资助项目(9140A160308HK61)

摘　　要：提出了一种基于多尺度网格误差分析的新型混合网格自适应局部加密策略。在初始网格基础上,通过多重网格计算,比较次细网格和细网格的计算结果,揭示出网格敏感区域,然后对这些网格敏感区域加密,计算自适应加密后的网格得到最终计算结果。相比于常规网格自适应策略,提出的新策略特别适合多种流动现象并存的高升力构型绕流流场计算中的敏感区域判断。NASA高升力全展构型的数值试验充分表明这种新策略的有效性。A new grid adaptation strategy based on multiscale grid error estimation is presented.By the information obtained in the full multigrid calculation on initial grid,we can quickly explore the critical local regions by comparing the solution of coarser and the fine grid,and then those regions are refined to generate the final grid and therefore the final computation is conducted on it.Other than conventional grid adaptation strategies,our strategy especially suit for the numerical simulation of high-lift configuration where several kinds of flow phenomena exist.The numerical experiments of NASA high-lift full-span configuration strongly show the efficient of our grid adaptation strategy.

关 键 词：粘流计算 网格自适应策略 NASA高升力全展构型 

分 类 号：V211.3[航空宇航科学与技术—航空宇航推进理论与工程]