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高速飞机的全机气动力数值分析
引用本文:李向群,安亦然,王世安,程暮林,张锡金,孙惠中.高速飞机的全机气动力数值分析[J].水动力学研究与进展(A辑),2004,19(Z1):838-848.
作者姓名:李向群  安亦然  王世安  程暮林  张锡金  孙惠中
作者单位:北京大学力学与工程科学系,北京,100871
摘    要:利用StarCD和FLUENT对一真实飞机模型进行了大量工况下的数值模拟,并将计算结果与试验结果进行了对比。根据计算的结果,论证了试验中存在的一些问题。最后将两种成品软件对同型号的飞机模拟结果对比,说明成品软件计算结果的准确性。

关 键 词:NS方程  全机数值模拟  动力影响  并行计算
文章编号:1000-4874(2004)增刊-0838-11
修稿时间:2004年2月15日

Numerical aerodynamic analysis of an high speed airplane
LI Xiang-qun,AN Yi-ran,WANG Shi-an CHENG Mu-lin,ZHANG Xi-jin,SUN Hui-zhong.Numerical aerodynamic analysis of an high speed airplane[J].Journal of Hydrodynamics,2004,19(Z1):838-848.
Authors:LI Xiang-qun  AN Yi-ran  WANG Shi-an CHENG Mu-lin  ZHANG Xi-jin  SUN Hui-zhong
Abstract:In this paper the real airplane computation was taken for massive flight conditions by using commercial code StarCD and Fluent, and the results were compared with relevant wind tunnel testing. According to the computation and analyzing, some wind tunnel testing defects were found. In order to make sure of the reliability of the code we used the part of cases was redone by another CFD code StarCD, and the consistency of the results was approved.
Keywords:NS-equation  numerical simulation  parallel computation
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