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CONTINUUM MECHANICS for ENGINEERS

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In a similar fashion, from dX (1) ⋅ dX (2) = dX (1) dX (2) cos Θ, where Θ is the angle<br />

between dX (1) and dX (2) , we obtain from Eqs 4.8-6 and 4.8-7,<br />

cos Θ =<br />

= λ λ nˆ c nˆ<br />

(4.8-15)<br />

( nˆ ) ( nˆ)<br />

1⋅ ⋅ 2<br />

which gives the original angle between elements in the directions and<br />

of the current configuration.<br />

ˆn 2<br />

Example 4.8-1<br />

A homogeneous de<strong>for</strong>mation is given by the mapping equations, x1 = X1 –<br />

X2 + X3, x2 = X 2 – X3 + X1, and x3 = X3 – X1 + X2 . Determine (a) the stretch<br />

ratio in the direction of Nˆ ˆ ˆ , and (b) the angle θ12 in the<br />

1 = ( I1+ I2)<br />

/ 2<br />

de<strong>for</strong>med configuration between elements that were originally in the directions<br />

of and .<br />

ˆ N ˆ ˆ<br />

1 N2 = I2<br />

Solution<br />

For the given de<strong>for</strong>mation (as the student should verify),<br />

(a) There<strong>for</strong>e, from Eq 4.8-4,<br />

and<br />

[ FiA]= 2<br />

Λ<br />

( Nˆ 1)<br />

Λ ( ˆ )<br />

N 1<br />

( 1)<br />

( 2)<br />

dX<br />

dX<br />

nˆ c nˆ<br />

1⋅ ⋅ 2<br />

⋅ =<br />

( 1)<br />

( 2)<br />

dX dX nˆ ⋅c⋅nˆ nˆ ⋅c⋅nˆ 1 2<br />

⎡ 1 −1<br />

1⎤<br />

⎢<br />

⎥<br />

⎢<br />

1 1 −1<br />

⎥<br />

⎣<br />

⎢−1<br />

1 1⎦<br />

⎥<br />

( )<br />

and<br />

1 1 2 2<br />

[ CAB]= ⎡ 3 −1 −1⎤<br />

⎢<br />

⎥<br />

⎢<br />

−1 3 −1<br />

⎥<br />

⎣<br />

⎢−1<br />

−1<br />

3⎦<br />

⎥<br />

⎡ 3 −1 −1⎤⎡1/<br />

2⎤<br />

⎢<br />

⎥ ⎢ ⎥<br />

= [ 1/ 2, 1/ 2, 0]<br />

⎢<br />

−1 3 −1<br />

⎥ ⎢1/<br />

2⎥=<br />

2<br />

⎣<br />

⎢−1<br />

−1<br />

3⎦<br />

⎥ ⎢<br />

⎣<br />

0 ⎥<br />

⎦<br />

=<br />

2<br />

(b) For ˆ ˆ 2<br />

N2 = I2<br />

, Λ so that from Eq 4.8-13, using the<br />

( ˆ = Iˆ ˆ<br />

I ) 2⋅C⋅ I2 = C22<br />

=<br />

3<br />

2<br />

result in part (a),<br />

ˆn 1

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