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大型捆绑式运载火箭气动特性数值模拟
引用本文:孙为民,谭发生,夏南.大型捆绑式运载火箭气动特性数值模拟[J].上海大学学报(自然科学版),2000,6(6):502-506,510.
作者姓名:孙为民  谭发生  夏南
作者单位:上海大学,上海市应用数学和力学研究所,上海,200072
摘    要:利用三维雷诺平均的Navier-Stokes方程,采用к-ε湍流模式,运用有限体积法,对某捆绑了4个助推器的大型运载火箭进行了计算,得到了火箭在亚、跨、超间速范围内的真实复杂流场所动特性。数值结果较好地反映了芯级和助推器之间的气动干扰状况。

关 键 词:NS方程  数值模拟  空气动力学  捆绑式运载火箭

Numerical Simulation of Aerodynamic Behavior of the Rocket with Four Boosters
SUN Wei-min,TAN Fa-sheng,XIA Nan.Numerical Simulation of Aerodynamic Behavior of the Rocket with Four Boosters[J].Journal of Shanghai University(Natural Science),2000,6(6):502-506,510.
Authors:SUN Wei-min  TAN Fa-sheng  XIA Nan
Abstract:A three-dimensional Reynolds averaged Navier-Stokes solver is applied to analyze the aerodynamic behavior of rocket with four boosters. The model employs the K--e model and relies on a finite volume method exploits grid refinement. A large amount of data have been attained describing the aerodynamic behavior of the configuration. The data reflects the interaction of a boundary layer on the rocket surface with a bow shock by the booster.
Keywords:numerical simulation of NS equation  aerodynamics of rocket  space technology  
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