Method for calculating fracture reliability of aircraft wing structure

The invention belongs to the field of aircraft damage tolerance analysis, and relates to an aircraft wing structure fracture reliability calculation method, which analyzes a wing structure hierarchical relationship according to aircraft wing structure parameters, and the described hierarchical relat...

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Bibliographic Details
Main Authors ZHU LIANG, NING YU, ZHANG YANJUN, LEI XIAOXIN
Format Patent
LanguageChinese
English
Published 08.07.2022
Subjects
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