Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology

<div>Change of AE hit number with the tensile loading time for matrix and interface damage in three specimens: (a) specimen of number 1; (b) specimen of number 2; (c) specimen of number 3.</div>

Shock and Vibration

fig9

Figure 9

Figure 9: Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology 