【摘要】 阐述了潜射导弹头体外形的气动与水动一体化设计方法 ,揭示了水下运动头部产生空化的机理 .根据理论与试验研究结果 ,分析了导弹出水过程中空泡溃灭对弹体的影响以及出水后导弹的气动特性更多还原

【Abstract】 The integrated design method of aerodynamics and hydrodynamics of nose shape is given, an investigation on the inciption and developing cativation of nose is also obtained. According to research result of theory and experimentation, the influence of cavitation losed in exiting water process of missile as well as some aerodynamics properties of missile is analysed.更多还原