1. Hart-Smith, L. J., Bolted Joints in Graphite/Epoxy Composites, NASA Cr-144899, National Aeronautics and Space Administration, Washington, DC, January 1977.
2. Agarwal, B. L., Static Strength Prediction of Bolted Joints in Composite Material, AIAA/ASME/ASCE/AHS. 20th Structure, Structural Dynamics and Material Conference, St. Louis, MO, April, 1979, pp. 303 - 309.
3. Oplinger, D. W., and Gandhi, K. R., Stresses in Mechanically Fastened Orthotropic Laminates, Proceedings of The Conference on Fibrous Composites in Flight Vehicle Design, Dayton, Ohio, 21-24 May, 1974, Air Force Flight Dynamics Laboratory Report No. AFFDL-TR-74-103, pp. 811 - 842.
4. Oplinger, D. W., Analytical Studies of Structural Performance in Mechanically Fastened Fiber-reinforced Plates, Proceedings of The Army Symposium on Solid Mechanics, 1974: The Role of Mechanics in Design - Structural Joints. Army Materials and Mechanics Research Center, Watertown, Mass., Report No. AMMRC MS 74-8, pp. 211 - 42.
5. Garbo, S. P. and Gallo, R. L., Strength of Laminates with Loaded Holes, presented at The 5th DOD/NASA Conference on Fibrous Composites in Structural Design, New Orleans, LA, January, 1981.