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AML parameter AML value applied load arc length Average Strain Index axial bearing failure bolted composite joint bolted joints bottom skins boundary conditions calculated Composite Materials compression loading computed Contour Plot Curved Panel deflected shape developed displacement edges equation Example failure analysis failure criterion failure load failure modes failure theory fiber breakage fiber-matrix compression failure fiber-matrix shearing finite element analysis Geodesic geometry hole boundary IM8/APC-HTA inches inplane input ISPAN module laminated composites LAMSTR layer limit point longitudinal margins of safety material properties matrix cracking mode of failure mode shape nonlinear NUMBER Panel Contour Plot Panel Strip plies ply orientation poisson's ratio post-buckling predicted failure Primary Aircraft Structures runstreams Shariffi and Sable shear loads shear modulus shear stresses shown in Figure solution specified static analysis stiffness Strain Index Values target point Task tensile test data TEXTJOINT top and bottom Truss Core Panel unidirectional composite Weibull distribution