摘要
研究机载布撒器绕流场的结构 ,为气动特性分析和外形改进提供依据 .以三维N S方程为出发方程 ,采用S A湍流模型 ,对机载布撒器的绕流场进行了数值模拟 .给出了流场图像和气动特性计算结果 ,并将气动特性计算结果与实验结果进行了比较分析 .气动特性计算结果与风洞实验结果基本吻合 。
Based on the three-dimension Navier-Stokes equations closed with Spalart-Allmaras(S-A) turbulence model, the computational fluid dynamics(CFD) numerical simulation was used to investigate the aerodynamic characteristics of stand-off air-to-surface dispenser. Through the simulation the flow field structures and computational aerodynamic characteristics were obtained. Computational aerodynamic characteristics were found to be in good agreement with wind tunnel test results. The numerical simulation results had been applied to analyze the aerodynamic characteristics and optimize the configuration of stand-off air-to-surface dispenser in engineering design.
出处
《弹道学报》
EI
CSCD
北大核心
2004年第4期33-37,共5页
Journal of Ballistics
关键词
机载布撒器
非圆截面弹身
气动特性
数值模拟
stand-off air-to-surface dispenser, noncircular cross-section missile, aerodynamic characteristics, numerical simulation