12 April 2012 Research of carbon composite material for nonlinear finite element method
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Proceedings Volume 8409, Third International Conference on Smart Materials and Nanotechnology in Engineering; 84092T (2012) https://doi.org/10.1117/12.923276
Event: Third International Conference on Smart Materials and Nanotechnology in Engineering, 2011, Shenzhen, China
Abstract
Works on the absorption of collision energy in the structural members are carried out widely with various material and cross-sections. And, with ever increasing safety concerns, they are presently applied in various fields including railroad trains, air crafts and automobiles. In addition to this, problem of lighting structural members became important subject by control of exhaust gas emission, fuel economy and energy efficiency. CFRP(Carbon Fiber Reinforced Plastics) usually is applying the two primary structural members because of different result each design parameter as like stacking thickness, stacking angle, moisture absorption ect. We have to secure the data for applying primary structural members. But it always happens to test design parameters each for securing the data. So, it has much more money and time. We can reduce the money and the time, if can ensure the CFRP material properties each design parameters. In this study, we experiment the coupon test each tension, compression and shear using CFRP prepreg sheet and simulate non-linear analyze at the sources - test result, Caron longitudinal modulus and matrix poisson's ratio using GENOAMQC is specialized at Composite analysis. And then we predict the result that specimen manufacture changing stacking angle and experiment in such a way of test method using GENOA-MCQ.
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Jung Ho Kim, Jung Ho Kim, Mohit Garg, Mohit Garg, Ji Hoon Kim, Ji Hoon Kim, "Research of carbon composite material for nonlinear finite element method", Proc. SPIE 8409, Third International Conference on Smart Materials and Nanotechnology in Engineering, 84092T (12 April 2012); doi: 10.1117/12.923276; https://doi.org/10.1117/12.923276
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