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Composites can be manufactured using either resin transfer ...

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Figure 6.5. FFT spectrum based on Abaqus results comparing the frequency response<br />

of a [06/904/06]T orientation undamaged coupon and a coupon with an em<strong>be</strong>dded crack<br />

in the middle four plies. ...........................................................................................................52<br />

Figure 6.6. Enlarged view of a FFT spectrum at frequencies near 976.6 Hz showing less<br />

than 2% difference <strong>be</strong>tween the frequency response of a [06/904/06]T orientation<br />

undamaged coupon and a coupon with an em<strong>be</strong>dded crack in the middle four plies. .............52<br />

Figure 6.7. Complete FFT spectrum for [016]T composite coupons comparing the<br />

frequency response of undamaged to damaged coupons that is provided by varying the<br />

depth of a surface crack. ..........................................................................................................53<br />

Figure 6.8. An enlarged view of FFT spectrum for an [016]T undamaged composite<br />

coupon and coupons with a surface crack of various depths for frequencies near: a)<br />

976.6 Hz and b) 7.617 kHz. ....................................................................................................54<br />

Figure 6.9. A graphical representation of RMS deviation <strong>be</strong>tween a [016]T undamaged<br />

coupon and coupons with a surface crack of various depths as a function of crack depth. .....55<br />

Figure 6.10. Complete FFT spectrum for [016]T composite coupons comparing the<br />

frequency response of an undamaged coupon to coupons with a four ply deep crack at<br />

various depths. .........................................................................................................................56<br />

Figure 6.11. An enlarged view of a FFT spectrum for an [016]T undamaged composite<br />

coupon and coupons with a four ply deep surface crack at various depths at frequencies<br />

near: a) 976.6 Hz and b) 7.617 kHz. ........................................................................................56<br />

Figure 6.12. A graphical representation of RMS deviation <strong>be</strong>tween a [016]T undamaged<br />

composite coupon and coupons with a four ply deep crack at various depths as a<br />

function of crack location. .......................................................................................................57<br />

Figure 6.13. Complete FFT spectrum for [016]T composite coupons comparing the<br />

frequency response of undamaged coupon to coupons with a four ply deep surface<br />

crack at various locations across the coupon. ..........................................................................58<br />

Figure 6.14. Enlarged view of FFT spectrum for an [016]T undamaged composite<br />

coupon and coupons with a four ply deep surface crack at various locations at<br />

frequencies near: a) 976.6 Hz and b) 7.617 kHz. ....................................................................59<br />

Figure 6.15. A graphical representation of RMS deviation <strong>be</strong>tween an [016]T undamaged<br />

composite coupon and coupons with a four ply deep surface crack at various locations<br />

across the coupon. ....................................................................................................................60<br />

Figure 7.1. A flow chart demonstrating the interface <strong>be</strong>tween MATLAB and Abaqus<br />

that used for generating data set for sensor placement optimization (where count is the<br />

iteration num<strong>be</strong>r). .....................................................................................................................62<br />

Figure 7.2. A FE representation of longitudinal strain component contour plot observed<br />

on the top surface of a composite coupon with an em<strong>be</strong>dded crack in the middle. .................63<br />

xiii

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