Aeroelastic Analysis of Perovskite Solar cell

该项目旨在开发一种新的计算框架来研究钙钛矿太阳能电池（PSC）复合结构的气动弹性行为。PSC作为一个潜在的颠覆性空间市场进入者，因其高比功率、灵活性和低制造成本而吸引了科学界和航空航天业。钙钛矿太阳能电池（PSC）的发现已成为第三代光伏器件的重大突破。由此产生的PSC的高比功率和灵活性减轻了卫星的有效载荷，同时增强了光伏系统部署的适应性。这些优势使革命性的PSC成为当代空间面板领域的一个很好的竞争对手。近年来，新兴的钙钛矿和有机太阳能电池技术引起了研究人员的广泛关注。应用于宇宙飞船或卫星，这种面板将节省推进剂，并为太空任务创造新的可能性。PSC产品在运行过程中，外界的意外影响普遍存在且不可避免，严重危及实际设备的使用寿命。在新型PSC成功的实际部署过程中，研究结构的动态力学性能和稳定性是一个紧迫而必要的问题。这种特性是空间结构设计的关键问题，也是对抗气动载荷的关键能力指标。相反，疏忽可能会导致复合材料降解和损坏，从而影响PSC结构的使用性能和安全性。因此，本研究旨在开发一个鲁棒有限元框架来研究PSC复合梁、板和复合壳结构的气动弹性行为。

This project aims to develop a novel computational framework to study the aeroelastic behaviour of perovskite solar cell (PSC) composite structures. The (PSC), as a potential disruptive space market entrant, has fascinated both the scientific community and the aerospace industry due to its high specific power, flexibility, and low fabrication cost. The perovskite solar cell (PSC) discovery has become a dominant breakthrough within third-generation photovoltaic devices. The resultant high specific power and flexible inherence of the PSC alleviate the satellite payload while strengthening the adaptability in deploying the photovoltaic system. These advantages qualify the revolutionary PSC as a good rival in the contemporary space panel sector. The emerging perovskite and organic solar cell technologies have recently attracted much attention among researchers. Applied in space crafts or satellites, such panels would save propellants and create novel possibilities for space missions. During the operation of the PSC products, the unanticipated external impacts are prevalent and inescapable, severely endangering the practical devices' serviceability. During the successful voyage towards practical deployment of the novel PSC, investigating the structure's dynamic mechanical performance and stability is an urgent and essential issue. Such an attribute represents a critical issue for space structure design and a crucial capability metric against aerodynamic loadings. On the contrary, negligence might yield composite degradation and damage, compromising the operational performance and safety of the PSC structure. Therefore, this research aims to develop a robust finite element framework to study the aeroelastic behaviour of PSC composite beams, plates and composite shell structures.