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Dynamics cheat sheet

my dynamics notes - 12000.org

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x 1<br />

x 2<br />

k 1 x 1<br />

k 2 x 2 x 1 <br />

m<br />

k 2 x 2 x 1 <br />

m 2<br />

1<br />

f 1 t<br />

f 2 t<br />

F m 1 x 1<br />

<br />

k 1 x 1 k 2 x 2 x 1 f 1 t m 1 x 1<br />

<br />

F m 2 x 2<br />

<br />

k 2 x 2 x 1 f 2 t m 2 x 2<br />

<br />

Hence, from the above the equations of motion are<br />

or<br />

In Matrix form<br />

⎡ ⎤ ⎧<br />

⎣ m 1 0 ⎨<br />

⎦<br />

0 m<br />

⎩<br />

2<br />

m 1 x ′′<br />

1 + k 1 x 1 − k 2 (x 2 − x 1 ) = f 1 (t)<br />

m 2 x ′′<br />

2 + k 2 (x 2 − x 1 ) = f 2 (t)<br />

m 1 x ′′<br />

1 + x 1 (k 1 + k 2 ) − k 2 x 2 = f 1 (t)<br />

m 2 x ′′<br />

2 + k 2 x 2 − k 2 x 1 = f 2 (t)<br />

x ′′<br />

1<br />

x ′′<br />

2<br />

⎫ ⎡<br />

⎤ ⎧ ⎫ ⎧ ⎫<br />

⎬<br />

⎭ + ⎣ k 1 + k 2 −k 2<br />

⎨x ⎦ 1 ⎬ ⎨<br />

−k 2 k<br />

⎩<br />

2 x<br />

⎭ = f 1 (t) ⎬<br />

⎩<br />

2 f 2 (t)<br />

⎭<br />

The above two EOM are coupled in stiffness, but not mass coupled. Using short notations, the above is<br />

written as<br />

[M]{x ′′ } + [K]{x} = {f}<br />

Modal analysis now starts with the goal to decouple the EOM and obtain the fundamental shape functions that<br />

the system can vibrate in. To make these derivations more general, the mass matrix and the stiffness matrix are<br />

written in general notations as follows<br />

⎡ ⎤ ⎧<br />

⎣ m 11 m 12<br />

⎨<br />

⎦<br />

m 21 m<br />

⎩<br />

22<br />

x ′′<br />

1<br />

x ′′<br />

2<br />

⎫ ⎡ ⎤ ⎧ ⎫ ⎧ ⎫<br />

⎬<br />

⎭ + ⎣ k 11 k 12<br />

⎨x ⎦ 1 ⎬ ⎨<br />

k<br />

⎩<br />

22 x<br />

⎭ = f 1 (t) ⎬<br />

⎩<br />

2 f 2 (t)<br />

⎭<br />

k 21<br />

The mass matrix [M] and the stiffness matrix [K] must always come out to be symmetric. If they are not<br />

symmetric, then a mistake was made in obtaining them. As a general rule, the mass matrix [M] is PSD (positive<br />

definite matrix) and the [K] matrix is positive semi-definite matrix. The reason the [M] is PSD is that x T [M]{x}<br />

represents the kinetic energy of the system, which is typically positive and not zero. But reading some other<br />

references 1 it is possible that [M] can be positive semi-definite. It depends on the application being modeled.<br />

1.2 Step 2, solving the eigenvalue problem, finding the natural frequencies<br />

The first step in modal analysis is to solve the eigenvalue problem det ( [K] − ω 2 [M] ) = 0 in order to determine<br />

the natural frequencies of the system. This equations leads to a polynomial in ω and the roots of this polynomial<br />

1 http://en.wikipedia.org/wiki/Fundamental_equation_of_constrained_motion<br />

4

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