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CONTINUUM MECHANICS for ENGINEERS

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x 1x 2 plane to be one of elastic symmetry. Accordingly, the elastic constant<br />

matrix <strong>for</strong> this case has the <strong>for</strong>m<br />

C C C C<br />

C C C C<br />

C C C C<br />

[ Cαβ<br />

] C C<br />

C C<br />

C C C C<br />

=<br />

⎡ 11 12 13 0 0 16 ⎤<br />

⎢<br />

⎥<br />

⎢ 21 22 23 0 0 26 ⎥<br />

⎢<br />

⎥<br />

31 32 33 0 0 36<br />

⎢<br />

⎥<br />

⎢ 0 0 0 44 45 0 ⎥<br />

⎢ 0 0 0 ⎥<br />

54 55 0<br />

⎢<br />

⎥<br />

⎣⎢<br />

61 62 63 0 0 66 ⎦⎥<br />

(6.3-6)<br />

and the original 36 constants are reduced to 20. Also, if a strain energy<br />

functions exists, C αβ = C βα and these 20 nonzero constants would be further<br />

reduced to 13.<br />

If the x 2x 3 plane is also one of elastic symmetry at the same time as the<br />

x 1x 2 plane at a point and we repeat the procedure outlined above, we find<br />

that C 16, C 26, C 36, C 45, C 54, C 61, C 62, and C 63 must also be zero, and the C matrix<br />

is further reduced to<br />

C C C<br />

C C C<br />

C C C<br />

[ Cαβ<br />

] C<br />

C<br />

C<br />

=<br />

⎡ 11 12 13 0 0 0 ⎤<br />

⎢<br />

⎥<br />

⎢ 21 22 23 0 0 0<br />

⎥<br />

⎢<br />

⎥<br />

31 32 33 0 0 0<br />

⎢<br />

⎥<br />

⎢ 0 0 0 44 0 0 ⎥<br />

⎢ 0 0 0 0 ⎥<br />

55 0<br />

⎢<br />

⎥<br />

⎣⎢<br />

0 0 0 0 0<br />

66 ⎦⎥<br />

(6.3-7)<br />

having 12 nonzero coefficients, or 9 if a strain energy function exists.<br />

Interestingly enough, if x 1x 3 is also a plane of elastic symmetry along with<br />

the two considered above, no further reduction in the C αβ matrix occurs. A<br />

material possessing three mutually perpendicular planes of elastic symmetry<br />

is called an orthotropic material, and its elastic constants matrix is that given<br />

in Eq 6.3-7.<br />

The reduction of the orthotropic elastic matrix to that of the isotropic<br />

matrix may be completed by successive consideration of the three axes of<br />

elastic symmetry shown in Figure 6-4 as well as their respective trans<strong>for</strong>mation<br />

matrices. By the rotation of 90° about the x 1 axis (Figure 6-4a), we find<br />

that C 12 = C 13, C 21 = C 31, C 22 = C 33, C 23 = C 32, and C 55 = C 66. For the rotation of<br />

90° about the x 3 axis (Figure 6.4b), we see that C 12 = C 21, C 11 = C 22, C 12 = C 23,<br />

C 31 = C 32, and C 44 = C 55. Finally, by a rotation of 45° about the x 3 axis<br />

(Figure 6-4c), we obtain 2C 44 = C 11 – C 12. There<strong>for</strong>e, by setting C 44 = µ and<br />

C 12 = λ, we may identify these remaining three C αβ’s with the Lamé constants<br />

and write the elastic coefficient matrix <strong>for</strong> isotropic behavior as

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