1. Tate MB, Rosenfeldt SJ. Preliminary investigation of the loads carries by individual bolts in bolted joints. Technical Report, NACA TN 1051, May 1946.
2. Nelson WD, Bunin BL, Hart-Smith LJ. Critical joints in large composite aircraft structure. Technical Report Company Paper DP 7266, Douglas Aircraft, January 1983. Also NASA CR-371, August 1983.
3. Stresses and displacements due to load transfer by fasteners in structural assemblies;Barrois;Eng Fract Mech,1978
4. A simple method for determining the effects of bolt-hole clearance on load distribution in single-column multi-bolt composite joints;McCarthy;Compos Struct,2005
5. Study of the behavior of a composite multi-bolt joint;Yang;Comput Struct,1990