摘要
本文给出一种较有效的多层网格构成形式,并提出“预测—修正”壁面边界处理法。通过采用当地时间步和引入余差光滑处理法,进一步提高了格式的收敛性和稳定性。作为算例,本文对二维无粘跨音速叶栅流动求解,计算结果与试验数据对比表明,本算法收敛快和计算精度好。
This paper gives an efficient form of multiple-grid scheme and presents a
'prediction-correction ' method for processing the boundary conditions on a solid wall. The conver-gency and the stability of the scheme can be further improved by using local time stepping and residual smoothing. Finally, two-dimensional inviscid transonic cascade flows are calculated. The comparison
between the calculated and the measured results shows that this scheme possesses very fast convergence speed and satisfactory accuracy.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1989年第3期228-232,共5页
Journal of Aerospace Power