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5003 Lectures - Faculty of Engineering and Applied Science

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E<strong>5003</strong> - Ship Structures I 112<br />

© C.G. Daley<br />

⎡k<br />

11 k 12 k 13 k 14 k 15 k 16 ⎤<br />

⎢<br />

⎥<br />

⎢<br />

k 21 k 22 k 23 k 24 k 25 k 26 ⎥<br />

⎢k<br />

⎥<br />

31 k 32 k 33 k 34 k 35 k 36<br />

K = ⎢<br />

⎥<br />

⎢k<br />

41 k 42 k 43 k 44 k 45 k 46 ⎥<br />

⎢k<br />

⎥<br />

51 k 52 k 53 k 54 k 55 k 56<br />

⎢<br />

⎥<br />

⎢⎣<br />

k 61 k 62 k 63 k 64 k 65 k 66 ⎥⎦<br />

We will now derive these 36 terms. Luckily they are not all unique.<br />

Axial Terms<br />

The axial terms are found by asking what set <strong>of</strong> forces is required to create a<br />

unit displacement at d.o.f. #1 (<strong>and</strong> only #1);<br />

For axial compression, the deflection under load is;<br />

F1L<br />

F1<br />

δ 1 = = 1⇒<br />

= k11<br />

=<br />

AE δ<br />

1<br />

AE<br />

L<br />

the force at d.o.f. #4 is equal <strong>and</strong> opposite to the force at #1;<br />

F<br />

4<br />

F 4<br />

= −F1<br />

⇒ = k 41<br />

δ<br />

There are no other forces (at #2, 3, 5, 6), so we have;<br />

1<br />

F 2 = k 21 = 0 <strong>and</strong> k 31 = k 51 = k 61 = 0<br />

δ1<br />

A displacement at 4 would require a similar set <strong>of</strong> forces, so that we can also<br />

write;<br />

=<br />

−<br />

AE<br />

L

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