机译:冲击损伤对采用GLARE粘结缓凝剂增强的结构疲劳性能的影响
Materials Engineering, The Open University, Walton Hall, Milton Keynes MK7 6AA, UK ,Faculty of Engineering and Computing, Coventry University, Priory Street, Coventry CV1 5FB, UK;
Faculty of Engineering and Computing, Coventry University, Priory Street, Coventry CV1 5FB, UK;
Materials Engineering, The Open University, Walton Hall, Milton Keynes MK7 6AA, UK;
School of Applied Sciences, Cranfield University, Bedfordshire MK43 0AL, UK;
School of Applied Sciences, Cranfield University, Bedfordshire MK43 0AL, UK;
Bonded crack retarders; Fatigue crack growth; Impact fatigue; Residual stresses;
机译:温度和热循环对GLARE粘结缓凝剂增强铝疲劳裂纹扩展的影响
机译:两种粘结缓凝剂增强的航空级铝合金疲劳裂纹扩展性能的比较。
机译:用粘结带加固的结构中的残余应力旨在抑制疲劳裂纹的增长
机译:飞机结构的寿命扩展技术 - 通过粘合裂隙延迟器延伸耐久性和促进损伤耐受性
机译:保温时间,热机械疲劳,喷丸和滞后对喷气发动机Inconel燕尾槽中疲劳裂纹扩展的影响的研究
机译:初始静载荷裂缝下钢纤维增强薄板轻质混凝土叠合梁的弯曲疲劳性能
机译:用粘结的缓凝剂增强的航空结构中的残余应力