Abstract
Composite panels are prone to delamination damage caused by impact or manufacturing process. This results in a local loss of stiffness in the panel where the delamination has occurred. The present study aims at taking advantage of full-field measurements and inverse identification procedures to solve this problem. A deflectometry technique [1] is employed to perform full-field slope measurements. The curvatures are then obtained from the slopes by numerical differentiation. The deflectometry setup is shown in Fig. 1.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Similar content being viewed by others
References
Avril S., Grédiac, M., Pierron F. and Surrel Y., In Proceedings of Xth SEM International Congress on Experimental Mechanics, Costa Mesa, USA, 2004.
Grédiac M., Toussaint E. and Pierron F., International Journal of Solids and Structures, vol. 39,2691–2705,2002.
Grédiac M., Toussaint E. and Pierron F., International Journal of Solids and Structures, vol. 40,2401–2419,2003.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2007 Springer
About this paper
Cite this paper
Kim, J.H., Pierron, F., Wisnom, M. (2007). Identification of the Local Stiffness Reduction of Damaged Composite Plates Using Full-Field Measurements. In: Gdoutos, E.E. (eds) Experimental Analysis of Nano and Engineering Materials and Structures. Springer, Dordrecht. https://doi.org/10.1007/978-1-4020-6239-1_335
Download citation
DOI: https://doi.org/10.1007/978-1-4020-6239-1_335
Publisher Name: Springer, Dordrecht
Print ISBN: 978-1-4020-6238-4
Online ISBN: 978-1-4020-6239-1
eBook Packages: EngineeringEngineering (R0)