복합재료역학 3장 레포트

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복합재료역학 3장 레포트

목차

3.9
3.10
3.11
3.12

본문내용

3.9 Write a computer program to read in the five engineering constants(, , , , and ) of a transversely isotropic material and calculate the individual terms of the compliance matrix [S] and the Stiffness matrix [C]. Calculate and print (in matrix form) the values of [S] and [C] for T200/5208 carbon/epoxy.

open(1, file=`C_T300.dat`)
open(2, file=`S_T300.dat`)

real E1, E2, N12, G12, N23, E3, N13, N31, N21, N32, G13, G23, delta, S(6,6), C(6,6)

N12=0.24
G12=0.82
N23=0.59
E1=19.2
E2=1.56

E3=E2
N21=N12*E2/E1
N32=N23
N13=N12
N31=N12*E2/E1
G13=G12
G23=E2/(2*(1+N23))

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