报告题目：A Lesson Learned from Composite Structure Design for Large Commercial Aircraft
报告人：牛康民，教授，北京科技大学
报告时间：2024年6月6日上午10:10
报告地点：江南网页版-江南（中国）纺织科学与工程学院6E112
内容简介：The successful development of all composite structure aircraft, for example well known Boeing's 787 and Airbus's A350 aircrafts, represents a revolutionary breakthrough in composite material technology. However, it is well recognized that the compressive strength of advanced resin-based composites is much lower than the tensile strength. The higher the fiber strength property, the greater the gap. The low compressive strength of high-performance carbon fiber reinforced polymer (CFRP) composites has been an issue in the companying composites industry for decades.
K Niu and R Talreja (2000) proposed a resin controlled yield criterion for the compressive failure of unidirectional fiber composites, which turned out to be in a very simple expression as the rule of mixtures for axial compression. The rule of mixtures is illustrated to show compressive failure of a fiber composite in this presentation.
报告人简介：牛康民，北京科技大学教授、博导、北科杰出学者、国家特聘专家，佐治亚理工大学Georgia Institute of Technology 航空工程博士；现任北科大复合材料结构工程中心主任；此前任西门子公司院士工程师，负责新一代大型燃气轮机叶片完整性和寿命方法包括高性能碳纤维树脂基复合材料和陶瓷基复合材料结构。曾任美国波音公司机体结构实验室结构技术负责人，做为波音民用飞机集团复合材料结构资深专家参与了最新型777X、787梦想飞机机翼和机身结构的设计、分析与试验。主导确立公司非线性有限元模型分析方法。
（撰稿：李磊 审核：刘雍）
纺织科学与工程学院
2024年6月3日
