基于FEM-SPH的铆接加筋板结构入水冲击流固耦合动态响应数值分析

NUMERICAL ANALYSIS OF FSI RESPONSE FOR RIVETED STIFFENED PANEL STRUCTURES SUBJECTED TO WATER ENTRY IMPACT BASED ON FEM-SPH COUPLING

  • 摘要: 针对航空器水上迫降和水空跨介质机动工况中铆接加筋板结构的入水抗冲击性能评估难题,该文提出基于FEM-SPH耦合算法的多尺度分析方法,系统研究铆接加筋板结构入水冲击的流固耦合响应与失效机理。通过建立全局流固耦合模型,模拟了5 m/s~30 m/s速度梯度(5 m/s为间隔)的冲击工况,并结合局部精细化校核分析,实现了从宏观动态响应到局部失效机制的多尺度解析。结果表明:蒙皮入水冲击响应呈现四阶段动态演化规律,即初始冲击波主导阶段、渐进屈曲发展阶段、水弹性回弹阶段及边界震荡衰减阶段。正交加筋板形成协同承力体系,其应力再分配机制具有显著速度相关性。铆钉连接部位呈现应力梯度效应与剪力敏感性,而铆钉材料刚度差异(Al-7075/10钢)对失效模式无显著影响。增加蒙皮厚度并未引起入水冲击力峰值的显著变化,但其对冲击力的波动形态产生了影响,同时有助于提高结构抵抗冲击载荷的能力。该研究构建的跨尺度分析框架,有效弥补了全局模型在局部失效表征中的局限性,为航空器适坠性设计与抗冲击优化提供了理论依据。

     

    Abstract: To address the challenge of evaluating water impact resistance of riveted stiffened panel structures for aircraft ditching and water-air cross-medium maneuvers, this study proposes a multiscale analysis methodology based on the FEM-SPH coupled algorithm. This approach systematically investigates the fluid-structure interaction (FSI) response and failure mechanisms of riveted stiffened panels during water entry. By establishing a global FSI model simulating impact velocities ranging from 5 m/s to 30 m/s (in 5 m/s increments) and incorporating localized refined verification analyses, a multiscale characterization bridging macroscopic dynamic responses and local failure mechanisms is achieved. Results indicate that the skin water impact response exhibits a four-phase dynamic evolution pattern: Initial shock wave-dominated phase, progressive buckling development phase, hydroelastic rebound phase, and boundary oscillation attenuation phase. Orthogonal stiffeners form a synergistic load-bearing system where their stress redistribution mechanism demonstrates significant velocity dependence. Riveted joints exhibit stress gradient effects and shear force sensitivity; However, material stiffness differences (Al-7075 vs. 10 steel) in rivets show negligible influence on failure modes. Increasing skin thickness yields no significant change in peak water impact force, yet modifies the oscillation pattern of the impact load while enhancing the structural resistance to impact loading. The cross-scale analysis framework established in this research effectively addresses the limitations of global models in characterizing local failures, providing theoretical foundations for aircraft crashworthiness design and impact resistance optimization.

     

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