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Journal of Intelligent Material Systems and Structures, Vol. 19, No. 3, 319-324 (2008) DOI: 10.1177/1045389X07083180 Prediction of Impact Forces on an Aircraft Composite WingAgency for Defense Development, Yuseong P.O. Box 35-7, 7-2, Daejeon, 305-600, Korea
Chungnam National University, 220 Gung-dong, Yuseong-gu, Daejeon, 305-765, Korea, igkim{at}cnu.ac.kr The capabilities for monitoring impact forces on an aircraft composite wing using impact response function (IRF) are examined. The IRF is derived based on the finite element method (FEM). Impact locations are identified by minimizing strain errors and force deviation errors. The reconstruction of impact forces are performed by computational inverse methods. The results of impact location identifications and impact force reconstructions are verified by numerical simulations using finite element analysis.
Key Words: structure health monitoring impact composite wing.
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