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带椭球形气囊航行体落水-上浮过程仿真

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针对水下发射模型试验中的模型低速落水问题,提出一种带椭球形气囊的航行体落水回收方案,两个气囊等距分布在航行体两侧,航行体与气囊之间用连接带相连。数值仿真基于Abaqus的耦合欧拉-拉格朗日方法,通过对比AUV头段入水的试验结果和仿真结果,验证数值方法的有效性。分析在不同姿态角和不同初始囊压的条件下,带气囊航行体低速落水后的运动过程、囊压变化以及连接带的受力情况。研究结果表明,航行体姿态角是影响落水-上浮过程的最重要因素,初始囊压次之;对于最大落水深度、囊压峰值、拉力峰值而言,趋于垂直落水的工况更加危险,最大落水深度为1。33 倍航行体长度,最大囊压为 3。7 倍基准囊压,连接带最大拉力为 2。2 倍航行体重力。这些结论可为航行体落水回收的方案设计与结构参数设计提供参考依据。
Simulation of Falling-floating Process of Vehicle with Ellipsoidal Airbags
A recovery scheme of vehicle with ellipsoidal airbags is proposed for the problem of model falling into the water at low speed in the underwater launch model test.The numerical simulation is based on Abaqus coupled Eulerian-Lagrangian method,and the effectiveness of the numerical method is verified by comparing the numerical and experimental results of the AUV head section entering into the water.The motion process of the vehicle with airbags entering the water at low speed,the change of airbag pressure and the force of the connecting belt under the conditions of different attitude angles and different initial airbag pressures are analyzed.The results show that the attitude angle of vehicle is the most important factor affecting the falling-floating process,followed by the initial airbag pressure.For the maximum depth of falling into the water,the peak value of airbag pressure and the peak value of pulling force,the condition that tends to fall vertically is more dangerous,the maximum depth of falling into the water is 1.33 times the length of vehicle,the maximum airbag pressure is 3.7 times the baseline airbag pressure,and the maximum pulling force of connecting belt is 2.2 times the gravity of vehicle.These conclusions can provide a reference for the design of recovery scheme and structural parameters for the vehicles falling into the water.

vehicleairbagwater-entry impactcoupled Eulerian-Lagrangian method

包健、马贵辉、孙龙泉、陈惟楚、李明

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哈尔滨工程大学 船舶工程学院 复杂动力学与控制创新中心,黑龙江 哈尔滨 150001

中国航发商用航空发动机有限责任公司,上海 200241

北京宇航系统工程研究所,北京 100076

航行体 气囊 落水冲击 耦合欧拉-拉格朗日方法

国家自然科学基金青年科学基金项目中国博士后科学基金特别资助项目国家自然科学基金企业创新发展联合基金重点支持项目

520010952022T150154U20B2005

2024

兵工学报
中国兵工学会

兵工学报

CSTPCD北大核心
影响因子:0.735
ISSN:1000-1093
年,卷(期):2024.45(1)
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