首页 | 本学科首页   官方微博 | 高级检索  
     检索      

非结构隐式方法在空心弹丸流场模拟中的应用
引用本文:任登凤,谭俊杰,张军.非结构隐式方法在空心弹丸流场模拟中的应用[J].力学与实践,2006,28(5):24-27.
作者姓名:任登凤  谭俊杰  张军
作者单位:1. 南京理工大学动力工程学院,南京,210094
2. 南京航空航天大学航空宇航学院,南京,210016
基金项目:国家自然科学基金项目(10476011)资助.
摘    要:采用非结构网格的LU-SGS隐式算法计算三维Euler方程,数值模拟了不同马赫数以及不同攻角下某空心弹丸绕流流场,分析了流场的波系结构及其升阻力特性,计算结果表明空心弹丸的阻力系数比同口径的普通弹丸的阻力系数大约小30%,空心弹丸的阻力系数以及升力系数随攻角的变化规律与普通弹丸一致.

关 键 词:非结构网格  LU-SGS隐式算法  数值模拟  空心弹丸  升力特性  阻力特性
收稿时间:2005-09-05
修稿时间:2006-01-24

FLOWFIELD CALCULATION OF HOLLOW PROJECTILE USING IMPLICIT METHOD BASED ON UNSTRUCTURED MESHES
REN Dengfeng,TAN Junjie,ZHANG Jun.FLOWFIELD CALCULATION OF HOLLOW PROJECTILE USING IMPLICIT METHOD BASED ON UNSTRUCTURED MESHES[J].Mechanics and Engineering,2006,28(5):24-27.
Authors:REN Dengfeng  TAN Junjie  ZHANG Jun
Institution:1.School of Power Engineering, NUST, Nanjing 210094, China;2.School of Astronautics, NUAA, Nanjing 210016, China
Abstract:The implicit LU-SGS scheme based on unstructured meshes is employed to solve three-dimensional Euler equations.The flow field of a hollow projectile is numerically simulated for different Mach number and different attack angle.Complicated flow structure and its lift and drag characteristics are discussed.The numerical results indicate that the drag coefficient of a hollow projectile is smaller by about 30 percent than that of a common projectile with the same diameter,and the correlations between the drag and the lift coefficients of the hollow projectile and the attack angle are in agreement with those of the common projectile.The results are relevant to engineering designs.
Keywords:unstructured  implicit LU-SGS scheme  hollow projectile lift  characteristic  drag characteristic
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号