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Air Force Materials angle anisotropic applied assumed ASTM STP average stress Boron boundary conditions compliance Composite Laminates Composite Materials compression containing circular holes crack tip damage deformation determined displacement elastic constants engineering constants experimental failure criterion fiber Force Materials Laboratory Fracture Mechanics fracture models Fracture Toughness given governing equations Graphite/Epoxy Laminates H.T. Hahn HALF CRACK LENGTH hole radius in-plane isotropic material LAMINATE CONFIGURATION laminates containing circular linear elastic master curve material system matrix Metal Matrix Composites mid-plane multiaxial notch sensitivity factor notched strength data obtained off-axis on-axis orthotropic material plane plate forces point stress Poisson's ratio Polyimide predictions PWG-fracture model relative notch sensitivity S.W. Tsai shear modulus shearing stress shown in Figures solution specimen stiffness strain energy stress components Stress Concentrations stress criterion stress-strain symmetric laminates Tensile tension tensor thermal tip damage zone transformation transverse Unidirectional values