刘海军, 王 聪, 邹振祝, 王本利, 王柏秋. 潜射导弹出筒过程肩空泡形态和水阻动力特性研究[J]. 工程力学, 2012, 29(7): 313-319. DOI: 10.6052/j.issn.1000-4750.2010.09.0699
引用本文: 刘海军, 王 聪, 邹振祝, 王本利, 王柏秋. 潜射导弹出筒过程肩空泡形态和水阻动力特性研究[J]. 工程力学, 2012, 29(7): 313-319. DOI: 10.6052/j.issn.1000-4750.2010.09.0699
LIU Hai-jun, WANG Cong, ZOU Zhen-zhu, WANG Ben-li, WANG Bai-qiu. RESEARCH ON CAVITATION SHAPE AND HYDRODYNAMIC DRAG PROPERTY OF SUBMARINE LAUNCHING MISSILE IN DEEP WATER[J]. Engineering Mechanics, 2012, 29(7): 313-319. DOI: 10.6052/j.issn.1000-4750.2010.09.0699
Citation: LIU Hai-jun, WANG Cong, ZOU Zhen-zhu, WANG Ben-li, WANG Bai-qiu. RESEARCH ON CAVITATION SHAPE AND HYDRODYNAMIC DRAG PROPERTY OF SUBMARINE LAUNCHING MISSILE IN DEEP WATER[J]. Engineering Mechanics, 2012, 29(7): 313-319. DOI: 10.6052/j.issn.1000-4750.2010.09.0699

潜射导弹出筒过程肩空泡形态和水阻动力特性研究

RESEARCH ON CAVITATION SHAPE AND HYDRODYNAMIC DRAG PROPERTY OF SUBMARINE LAUNCHING MISSILE IN DEEP WATER

  • 摘要: 该文采用多相流模型、Singhal空化模型和动网格技术,对潜射导弹垂直发射出筒过程进行了数值模拟,并将仿真结果与文献数据进行了对比分析,二者具有较好的吻合性,验证了数值计算方法的准确性。得到了潜射导弹的肩部空泡几何形态和出筒过程的压力分布情况,获得了导弹的压差阻力系数曲线、摩擦阻力系数曲线和总阻力系数曲线,分析了肩空泡对潜射导弹的水阻动力特性的影响。

     

    Abstract: The underwater motion process of a submarine vertically launched missile from the tube in deep water was simulated by using a multiphase flow model, a Singhal cavitation model and dynamic mesh technique. The pressure drag coefficient of numerical results, being consistent with the references date as well, is compared with reference data, and the accuracy of the numerical method is demonstrated too. During the process of vertically launching from the tube, the shoulder cavitation geometric shape and the pressure distribution of submarine missile were obtained, the curves of pressure drag coefficients, friction drag coefficients and total drag coefficients were depicted, and the influence of shoulder cavitation to the hydrodynamic drag property of the submarine launching missile in deep water was analyzed.

     

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