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Determination of the Fracture Parameters in a Stiffened Composite Panel

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Figure

Figure 2.3 The schematic finite element mesh near a segment of the crack front.
Figure 3.1 Auxiliary line load on a three-dimensional crack: (a) uniform forces f 1
Figure 5.1 A through-thickness center-cracked plate subjected to a uniform far-field displacement.
Figure 5.3 Finite element mesh of a one-eighth center-cracked plate (a/w=0.1).
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ANSYS Program FORTRAN Program

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