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smart technologies for safety engineering

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24 Smart Technologies <strong>for</strong> Safety Engineering<br />

EA<br />

4 4<br />

t<br />

F.(t)<br />

0<br />

4<br />

t<br />

1<br />

4<br />

EA<br />

4 4<br />

t<br />

F.(t)<br />

t<br />

Figure 2.7 Impulse virtual distortion in an element, showing the process of matrix B ε , D ε composition<br />

capturing the influence of inertia on structural response. Again, the response of the structure<br />

to the impulse <strong>for</strong>ce distortion at nodes is obtained by the Newmark algorithm.<br />

It will be demonstrated in subsequent sections that by establishing the influence matrices B ε ,<br />

D ε , B f , D f , the remodeling of stiffness and mass in the structure becomes feasible. A nonlinear<br />

constitutive relation can also be accounted <strong>for</strong>. However, linear geometric relations (small<br />

strains) are assumed. Examples of VDM applications in dynamics are demonstrated in Chapters<br />

3 and 6.<br />

2.5.2 Stiffness Remodeling in Dynamics<br />

In signal processing per<strong>for</strong>med in many fields of <strong>engineering</strong>, the output response of a system<br />

is expressed as an integral of the product of the input excitation and transfer function (i.e. the<br />

system’s response to an impulse function like Dirac’s delta) over some period of time.<br />

For a simple harmonic oscillator of mass m and natural frequency ω, the convolution of the<br />

two functions determines the displacement u(t) due to a series of impulses f (τ)dτ over the<br />

1<br />

3<br />

4<br />

1<br />

3<br />

5<br />

4<br />

2<br />

1<br />

2<br />

t<br />

F.(t)<br />

0<br />

p 4x=1<br />

t<br />

Figure 2.8 Impulse virtual distortion at a node, showing the process of matrix B f , D f composition<br />

1<br />

1<br />

3<br />

3<br />

4<br />

4<br />

1<br />

1<br />

3<br />

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5<br />

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0<br />

p 4y=1<br />

4<br />

2<br />

4<br />

2<br />

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2<br />

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