基于一体化设计的气动外形参数对动态特性的影响

Influence of Aerodynamic Shape Parameters on the Dynamic Characteristics of Missiles Based on Integrated Design

  • 摘要: 为了提高导弹气动外形方案设计效率和设计质量,基于一体化设计方法,将导弹气动外形设计与气动特性计算、弹道仿真和飞行过程的动态特性分析等工作结合起来,分析导弹外形参数、气动力系数、动力系数、飞行动态性能参数之间的相互关系,得出部分主要气动外形参数对飞行动态特性典型参数的影响规律. 仿真与计算结果验证了通过改变气动外形参数来改变弹体动态特性参数的理论分析.

     

    Abstract: To enhance the efficiency and quality of aerodynamic shape scheme design of missiles, the aerodynamic shape design, aerodynamic characteristics estimation, trajectory simulation and dynamic characteristics analysis are combined based on integrated design. The correlations among aerodynamic shape parameters, aerodynamic coefficients, dynamic coefficients and dynamic characteristics parameters are analyzed, and the rule how the aerodynamic shape parameters affect dynamic characteristics parameters is studied. The conclusion that the dynamic characteristics parameters can be changed by changing relevant aerodynamic shape parameters is verified by calculation and simulation.

     

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