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气动热数值模拟中壁面热流后处理方法
引用本文:张胜涛,陈方,刘洪.气动热数值模拟中壁面热流后处理方法[J].航空动力学报,2014,29(11):2652-2658.
作者姓名:张胜涛  陈方  刘洪
作者单位:上海交通大学 航空航天学院, 上海 200240;上海交通大学 航空航天学院, 上海 200240;上海交通大学 航空航天学院, 上海 200240
基金项目:国家自然科学基金(11102111)
摘    要:针对气动热数值模拟中壁面热流后处理方法进行了系统的数值研究,提出了一种有别于常规微分法和积分法的壁面热流后处理方法.通过3种算例进行了对比分析,结果表明:即使在流场参数相同情况下,采用不同的壁面热流后处理方法计算的热流结果也会有较大差异,且表现出不同的网格依赖性.微分法对网格的依赖性较大,单纯提高差分精度不一定能够减弱网格依赖性和提高计算精度,还与近壁处网格分布密切相关;积分法从能量平衡积分方程出发,极大地减弱了网格依赖性,具有较高的计算精度.所提出方法具有与积分法相当的网格依赖性和计算精度,尤其在驻点区域,其网格依赖性更弱于积分法,且计算简单,提高了计算效率.

关 键 词:壁面热流后处理方法  高超声速  气动热  网格尺度  计算流体力学
收稿时间:2013/7/26 0:00:00

Post-processing methods for wall heat-flux in aeroheating numerical simulation
ZHANG Sheng-tao,CHEN Fang and LIU Hong.Post-processing methods for wall heat-flux in aeroheating numerical simulation[J].Journal of Aerospace Power,2014,29(11):2652-2658.
Authors:ZHANG Sheng-tao  CHEN Fang and LIU Hong
Institution:School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China;School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China
Abstract:A systematic study of post-processing methods for wall heat-flux in aeroheating numerical simulation was conducted and a post-processing method differing from conventional differential or integral methods was proposed. The comparisons among different post-processing methods were done by three cases. The results indicate that, even if the flow parameters remain the same, significant differences and grid-dependence in wall heat-flux prediction are observed using different post-processing methods. The differential method depends strongly on the grid used in calculations. Enhancement of the order of finite difference cannot always weaken its grid-dependence and improve its accuracy in wall heat-flux prediction, which is also related closely to the grid distribution near the wall. The integral method derived directly from the integral energy balance equation can significantly achieve a lower grid-dependence and thus a high accuracy. The proposed method can be compared with the integral method in the aspect of grid-dependence and accuracy. Especially, in the stagnation region, it has even weaker gird-dependence. Moreover, it is simpler and easier to be implemented numerically, thus further improving the computation efficiency.
Keywords:post-processing method for wall heat-flux  hypersonic  aeroheating  grid scale  computation fluid dynamics
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