机译:用弹道极限方程预测蜂窝夹芯板的穿孔响应
Missouri University of Science and Technology, Rolla, Missouri 65409;
Fraunhofer Institute for High-Speed Dynamics, 79104 Freiburg, Germany;
Fraunhofer Institute for High-Speed Dynamics, 79104 Freiburg, Germany;
d_c: critical projectile diameter for failure of rear wall, cm; d_p: projectile diameter, cm; K_(MLI): adjustment factor for multilayer insulation; K_(S2): adjustment factor for scaling standoff distance S_2 in the hypervelocity regime; K_m : adjustment factor for equipment cover plate thickness t_w in the hypervelocity regime; et al;
机译:用弹道极限方程预测蜂窝夹芯板的穿孔响应
机译:铝合金三明治面板与蜂窝核心的弹道冲击行为:实验研究
机译:铝合金三明治面板与蜂窝核心的弹道冲击行为:实验研究
机译:铝蜂窝夹层面板的弹道极限等式
机译:复合板和夹心板在准静态冲头和弹丸载荷下的穿孔。
机译:通风Ti-6AL-4V蜂窝夹芯板的高温机械性能
机译:平面内高速冲击下蜂窝夹层面板的抗坏焰抗性