摘要
推导了适合多组分含化学反应火箭燃气射流场对流项的ＴＶＤ数值格式及流动求解的组合格式，给出了某火箭燃气自由射流流场的计算结果。
TVD scheme for convection and assorted scheme,which is suitable for the flow of rocket gas efflux with multispecies and chemical reaction,have been deducted.Computational result of free efflux field for one rocket motor has been presented.
出处
《宇航学报》
EI
CAS
CSCD
北大核心
1998年第2期48-54,共7页
Journal of Astronautics
