A method to apply structure relevant impact damage to small structure relevant specimens for damage tolerance studies
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Abstract
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Research context
OpenAlex topics: Fatigue and fracture mechanics · High-Velocity Impact and Material Behavior
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References (5)
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1. Labonté, S. and Wiggenraad, J. F. M., ‘Development of a Structure Relevant Specimen for Damage Tolerance Studies’,9th International Conference on Composite Materials (ICCM-9). Madrid, Spain, 12–16 July, 1993.
2. Labonté, S. and Wiggenraad, J. F. M., ‘A Damage Tolerance Study Conducted with Structure Relevant Specimens’,NLR TP 93067 L, 1993.
3. Arendsen, P., Thuis, H. G. S. J. and Wiggenraad, J. F. M., ‘Optimization of Composite Stiffened Panels with Postbuckling Constraints’,CADCOMP 94, Southampton, U.K., 1994.
4. McCarty, J. E. and Roeseler, W. G., ‘Durability and Damage Tolerance of Large Composite Primary Aircraft Structure’,NASA CR-003767, 1984.
5. Zhang, X. and Davies, G. A. O., ‘Low Velocity Impact Damage in Stiffened CFRP Panels’. Imperial College of Science, Technology and Medicine, Aronautics Department, London, U.K. 1994.