Prediction of Impact Forces on an Aircraft Composite Wing
Source abstract
Abstract
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.
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Research context
OpenAlex topics: Structural Health Monitoring Techniques · Aeroelasticity and Vibration Control · Advanced Measurement and Detection Methods
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Affiliations
Agency 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,
References (11)
Show source-provided references
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