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[1]yuzhefeng. 机翼结构试验杠杆系统位移计算和参数化建模 实验室研究与探索, 2019,
[2]yuzhefeng. Hyperelastic analysis of pneumatic artificial muscle with filament-wound sleeve and coated outer layer Smart Materials and Structures , 2019,
[3] 基于内翻复合材料管的冲击吸能器特性研究 振动与冲击, 2018,
[4] 防撞柱结构抗冲击性能的落锤测试方法 全国固体力学会议, 2018,
[5]yuzhefeng. 含分层损伤复合材料层压板低速冲击模型刚度计算方法 复合材料学报, 2018,
[6] 复合材料层压板小质量冲击下分层扩展的接触力阈值识别 振动与冲击, 2018,
[7]yuzhefeng. Identification of threshold load causing the delamination growth in composite laminates subjected to small mass impact ZHENDONG YU CHONGJI/JOURNAL OF VIBRATION AND SHOCK, 2018,
[8] Shock Absorber Using Inward-folding Composite Tube and Its Application to a Crew Seat: Numerical Simulation The International Conference on Aerospace System Science and Engineering, 2018,
[9]yuzhefeng. Detection of Acoustic Emission Signal due to Impact Damage of Composite Materials based EMD The International Conference on Aerospace System Science and Engineering, 2018,
[10] 复合材料层压板小质量冲击下分层扩展的接触力阈值识别 振动与冲击, 2017,
[11] 基于内翻复合材料管的冲击吸能器特性研究 振动与冲击, 2017,
[12] 复合材料壁板结构低速冲击测试、建模与损伤准则 第三届中国国际复合材料科技大会, 2017,
[13] Experimental determination of delamination threshold load for small-mass impact on composite laminates 20th International Conference on Composite Structures (ICCS20), 2017,
[14] Stiffness Reduction Due to Delamination Onset for the Simulation of Low Velocity Impact on Composite 20th International Conference on Composite Structures (ICCS20), 2017,
[15] Damage resistance of a co-cured composite wing box to low-velocity impact Composite Structures, 2017,
total72 2/5
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