为了满足新一代空天飞行器的超轻结构设计(超轻质、高强度、高韧度和防湿热)、结构大尺度展缩与控制和可靠运行的主动控制和智能监测的多功能化要求,迫切要求发展新型的轻质多材料,建立完整的理论体系来描述其不同功能及相应的指标参数,以催生崭新的设计理念和实施制备方案并带动新材料新功能的孕育。本课题的任务和目标在于表征点阵材料的本构模型和失效机理;结合新一代空天飞行器的结构设计实现汇材料设计、结构设计和功能设计为一任的协同优化设计理念;探讨基于点阵材料夹芯的复合结构材料制备技术。
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数据更新时间:2023-05-31
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