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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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
08.07.2022
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Subjects | |
Online Access | Get full text |
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