Nondestructive Damage Evaluation in Ceramic Matrix Composites for Aerospace Applications

<table>Dissipated energy versus % <svg height="12.3375" id="M19" style="vertical-align:-3.40976pt" version="1.1" viewbox="0 0 32.087502 12.3375" width="32.087502" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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q0 -61 24.5 -96.5t65.5 -35.5q51 0 87.5 46.5t50.5 100.5t14 102z" id="x1D70E"></path></g>
<g transform="matrix(.012,-0,0,-.012,9.663,12.112)"><path d="M716 650v-28q-46 -3 -65 -15.5t-22 -43.5q-6 -54 -6 -162v-82q0 -184 -75 -264q-68 -69 -180 -69q-98 0 -160 48q-88 67 -88 238v249q0 66 -13.5 81t-73.5 20v28h258v-28q-59 -4 -72.5 -19t-13.5 -82v-227q0 -122 48 -188t140 -66q189 0 189 286v75q0 111 -7 165
q-4 29 -24 40.5t-73 15.5v28h238z" id="x55"></path></g><g transform="matrix(.012,-0,0,-.012,18.42,12.112)"><path d="M495 163l30 -6q-19 -99 -36 -157h-453v28q63 5 77.5 20t14.5 78v400q0 63 -13 77t-75 19v28h261v-28q-61 -5 -74.5 -19t-13.5 -77v-395q0 -41 5 -59t18 -25q24 -13 96 -13q85 0 112 31q30 33 51 98z" id="x4C"></path></g><g transform="matrix(.012,-0,0,-.012,24.072,12.112)"><path d="M592 498l-30 -3q-13 63 -31 89q-13 19 -33.5 25.5t-75.5 6.5h-70v-493q0 -60 16 -75.5t86 -19.5v-28h-286v28q68 4 83.5 19.5t15.5 75.5v493h-62q-60 0 -83 -7t-33 -24q-12 -17 -32 -90h-29q10 116 12 180h20q10 -16 21 -20.5t34 -4.5h395q19 0 28.5 5t21.5 20h21
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</svg> for fatigue-loaded SiC/BMAS.</table>

The Scientific World Journal

fig8

Figure 8

Figure 8: Nondestructive Damage Evaluation in Ceramic Matrix Composites for Aerospace Applications 