Question: Given a carbon / epoxy composite panel under uniaxial loading, i . e . , = 0 , y y = 0 , plot x

Given a carbon/epoxy composite panel under uniaxial loading, i.e.,=0,yy=0, plot xy as a function of
fiber orientation going from 0 to 180 degrees. Material properties are given by: E1=140GPa,E2=10GPa,
G12=7GPa, and
u?(()()12)=0.3
Hint(s): For =35,xy=-0.04870.
Given a carbon / epoxy composite panel under

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