Volume 41 Issue 3
Mar.  2021
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YAO Xiongliang, WANG Zhi, YE Shanjun, WU Ziqi, WANG Zhikai. A simplified theoretical model for attack angle change of a hemispherically-nosed projectile while penetrating the stiffener of a ship plate frame[J]. Explosion And Shock Waves, 2021, 41(3): 033301. doi: 10.11883/bzycj-2020-0092
Citation: YAO Xiongliang, WANG Zhi, YE Shanjun, WU Ziqi, WANG Zhikai. A simplified theoretical model for attack angle change of a hemispherically-nosed projectile while penetrating the stiffener of a ship plate frame[J]. Explosion And Shock Waves, 2021, 41(3): 033301. doi: 10.11883/bzycj-2020-0092

A simplified theoretical model for attack angle change of a hemispherically-nosed projectile while penetrating the stiffener of a ship plate frame

doi: 10.11883/bzycj-2020-0092
  • Received Date: 2020-03-30
  • Rev Recd Date: 2020-11-29
  • Available Online: 2021-01-25
  • Publish Date: 2021-03-10
  • At present, there is no theoretical model for the influence of stiffeners on the impact angle and attack angle of a projectile penetrating a ship plate frame. In this paper, the problem of the rigid hemispherical nosed projectile penetrating the stiffener of the ship's plate frame is studied to give theoretical solution of the change of the attack angle. The stiffener is simplified as a rigid-plastic beam, the motion of which is controlled by plasto-dynamic equations of small deformation. By solving the coupled kinetic equations of the projectile and the beam, the deflection of the beam and the motion of the plastic hinges are obtained. The fracture of the beam is assumed to occur when the maximum tensile strain of the beam reaches the fracture strain of the material. By the above methods, the mechanical model of the penetration process is established. The formulas for the residual velocity, the change of impact angle, and the change of attack angle of the projectile are given. The formulas show that the change of impact angle and attack angle is related to the initial velocity, initial impact angle, initial attack angle, and the ultimate moment of the stiffener. By programming the theoretical formula, it is found that the influence of initial impact angle on the change of impact angle and attack angle at the end of penetration is greater than that of the initial attack angle. When the initial impact angle exceeds a certain value, the change of attack angle will increase dramatically. When the initial impact angle exceeds another limit value, the projectile will ricochet. A higher initial velocity corresponds to a smaller change of the impact angle and the attack angle. The ultimate moment of the stiffener has an important influence on the change of the attack angle.
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