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机译:膜充气锥弯曲时的初始起皱及其演变
Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;
Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;
Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;
membrane; inflated cone; wrinkling; extremum method; load-carrying efficiency;
机译:弯曲状态下长充气截锥的皱纹演变
机译:网状增强膜充气梁在弯曲作用下的起皱和塌陷
机译:弯曲和剪切作用下部分起皱的圆柱充气梁的数值分析
机译:膜膨胀锥棘锥的皱纹特征
机译:弯曲,翻边和深冲的力学原理以及计算机辅助建模系统,用于预测钣金成形中的应变,断裂,起皱和回弹。
机译:充气梁的交互式弯曲起皱行为
机译:充气梁的交互式弯曲起皱行为
机译:细长膨胀锥的线性化牛顿空气动力学。