Nonlinear dynamic response analysis of supercavitating vehicles

被引:0
|
作者
麻震宇 [1 ]
林明东 [1 ]
胡凡 [1 ]
张为华 [1 ]
机构
[1] College of Aerospace and Material Engineering,National U niversity of Defense Technology
关键词
supercavitating vehicle; shell element of relative degrees of freedom; nonlinear finite element; dynamic response;
D O I
暂无
中图分类号
U661.1 [船舶流体力学];
学科分类号
摘要
A finite element model for the supercavitating underwater vehicle was developed by employing 16-node shell elements of relative degrees of freedom.The nonlinear structural dynamic response was performed by introducing the updated Lagrangian formulation.The numerical results indicate that there exists a critical thickness for the supercavitating plain shell for the considered velocity of the vehicle.The structure fails more easily because of instability with the thickness less than the critical value,while the structure maintains dynamic stability with the thickness greater than the critical value.As the velocity of the vehicle increases,the critical thickness for the plain shell increases accordingly.For the considered structural configuration,the critical thicknesses of plain shells are 5 and 7 mm for the velocities of 300 and 400 m/s,respectively.The structural stability is enhanced by using the stiffened configuration.With the shell configuration of nine ring stiffeners,the maximal displacement and von Mises stress of the supercavitating structure decrease by 25% and 17% for the velocity of 300 m/s,respectively.Compared with ring stiffeners,longitudinal stiffeners are more significant to improve structural dynamic performance and decrease the critical value of thickness of the shell for the supercavitating vehicle.
引用
收藏
页码:2502 / 2513
页数:12
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