(2025). Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model. Fatigue of Aircraft Structures.
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Chicago Style (17th ed.) Citation
"Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model."
Fatigue of Aircraft Structures 2025.
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MLA (9th ed.) Citation
"Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model."
Fatigue of Aircraft Structures, 2025.
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Warning: These citations may not always be 100% accurate.