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Aeronautics and Space agrees with Westergaard's Alexander Mendelson AlOa central crack colinear cracks compatibility equation containing a central CONTAINING A CRACK cosh crack length crack opening v(x,0 crack under tension ELASTIC STRESS DISTRIBUTION equa equations 16 equations A3 factor is independent finite Fourier transforms finite-width orthotropic plate Fourier series Fourier sine transform given by equations infinite plate infinity integral equation isotropic plate jt(v kernel length to plate m*x m=l Mendelson and Samuel mitx mjtx NASA NASA TN NASA TECHNICAL NOTE normal stress distribution ORTHOTROPIC PLATE CONTAINING OTS price performed on equation plate width approaches ratio of crack set of colinear shown in appendix singular solution agrees solution reduces Space Administration Spero stress intensity factor substituted into equation Sxy(x,y sy,c TECHNICAL NOTE D-2260 tension is presented tion transform is performed well-known solution Westergaard's semi-inverse solution Westergaard's solut width approaches zero WIDTH ORTHOTROPIC PLATE x)sinh zero result