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.