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兵工学报 ›› 2013, Vol. 34 ›› Issue (5): 535-540.doi: 10.3969/j.issn.1000-1093.2013.05.004

• 研究论文 • 上一篇    下一篇

空心弹的阻力特性与气动外形数值分析

黄振贵, 李艳玲, 陈志华, 郭玉洁   

  1. 南京理工大学瞬态物理国家重点实验室, 江苏南京290014
  • 上线日期:2013-07-22
  • 作者简介:黄振贵(1986—),男,博士研究生
  • 基金资助:

    瞬态物理国家重点实验室基金项目(9140C300205110C30)

Numerical Investigations on the Drag and Aerodynamic Characteristics of a Hollow Projectile

HUANG Zhen-gui, LI Yan-ling, CHEN Zhi-hua, GUO Yu-jie   

  1. Key Laboratory of Transient Physics,Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China
  • Online:2013-07-22

摘要:

为了得到具有最小阻力系数的空心弹外形,基于雷诺平均方程以及二阶AUSM 格式,对不同空心弹气动外形的二维流场以及气动力进行了数值计算,得到了不同外形条件下空心弹的内外流场特性,以及阻力系数变化曲线与最小阻力系数的空心弹气动外形。另外,分别对具有最小阻力系数的空心弹与常规空心弹的超声速流场进行了数值模拟,对比分析了二者流场结构的异同,数值验证了具有最小阻力系数弹型的减阻效果,可为相关研究提供参考。

关键词: 流体力学, 空心弹, 管式弹, 阻力系数, 流场

Abstract:

With the purpose of obtaining the minimum drag coefficient of a normal hollow projectile, based on RANS governing equations and 2nd-order AUSM scheme, the two-dimensional flow fields and aerodynamic forces of different shapes of hollow projectiles have been simulated numerically, both the ex- ternal and internal flow features of hollow projectiles with different shapes are obtained, as well as the drag variation curves and the aerodynamic shape of the hollow projectile with the minimum drag coeffi- cient. Moreover, the projectile with minimum drag coefficient and normal projectile with ultrasonic sound flow fields are simulated respectively, the flow characteristics of them are discussed and compared, and the minimum drag effect of the obtained projectile is validated, our numerical results can provide impor- tant guidance for relative investigations.

Key words: fluid mechanics, hollow projectile, tubular projectile, drag coefficient, flow field

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