Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model

The increasing demand for greener aviation technology has driven the adoption of advanced composite materials in aircraft structures, offering significant weight saving and fuel efficiency improvements. Wing structures made of torsion boxes composed of stiffened panels have shown over the decades th...

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Principais autores:	Morlet Benoît, Congourdeau Fabrice, Sola Guy, Martini Dominique, Robin Alban, Jacques Vincent
פורמט:	Artigo
שפה:	Inglês
יצא לאור:	Sciendo 2025-07-01
סדרה:	Fatigue of Aircraft Structures
נושאים:	composite damage model stiffened panel post-bucking
גישה מקוונת:	https://doi.org/10.2478/fas-2024-0004
תגים:	הוספת תג אין תגיות, היה/י הראשונ/ה לתייג את הרשומה!