Progressive failure analysis of helicopter rotor blade under aeroelastic loading
作者： Kamran Ahmad , Yasir Baig , Hammad Rahman , Hassan Junaid Hasham
DOI: 10.3846/AVIATION.2020.12184
关键词:
摘要: … in the weakest ply exceed the allowable strength of the laminate. … to take the load till the updated strength is reached. In the … been used to model geometry of helicopter rotor. Under the …
narcis.nl参考文章(38)
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