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双组尾翼弹气动特性计算与分析 被引量:5

Aerodynamic character calculation and analysis of two sets of empennages bullet
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摘要 本文根据双组尾翼弹的外形特点,选用了代数网格生成方法,通过求解N S方程,对其气动特性进行了数值计算,并对其计算结果进行了分析。由计算结果可知,此种弹的双尾翼可以为其提供一定的转速和升力,提高其静稳定性。并且此种弹已经用于型号设计。 Based on the character of the shape of two sets of empennages bullet, this paper has given its calculation and analysis. It has chosen the algebraic grid generation and calculated the N-S equation to get the aerodynamic coefficients. 32 kinds of states, whose Mach number is 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, and attack angle is 0°, 2°, 4°, 6° have been calculated. According to the results and its graphs, it can be seen that the double empennages, especially its character of oblique, can offer rotation voltage and lift force, and this can increase its stability. In addition, this kind of bullet has been applied to model design.
出处 《空气动力学学报》 EI CSCD 北大核心 2002年第4期411-415,共5页 Acta Aerodynamica Sinica
关键词 双组尾翼弹 气动特性 计算 N-S方程 two sets of empennages bullet grid generation N-S equation aerodynamic character
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参考文献3

  • 1JAMESON A. Artificial diffusion, upwind biasing, limiters and their effect on accuracy and multi-grid convergence in transonic and hypersonic flows[R]. AIAA paper 93-3359.
  • 2张维全,周南等. 弹箭空气特性分析与计算[M]. 第一版,北京:国防工业出版社,1975.
  • 3武频,赵润祥,谭俊杰,郭锡福.滑翔增程弹气动特性分析[J].弹道学报,2001,13(4):38-41. 被引量:4

二级参考文献3

  • 1Jameson A. Artificial diffusion, upwind biasing, Limiters and their effect on accuracy and multi-grid convergence in transonic and hypersonic flows. AIAA paper: 93-3359
  • 2张维全,周南.弹箭空气特性分析与计算.北京:国防工业出版社,1975
  • 3赵润祥,陈少松,崔龙波,康九生,武频,谭俊杰.迫击炮弹气动力三维数值模拟[J].弹道学报,1999,11(2):58-61. 被引量:6

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