1. and “Prototype Development of an Optimized, Tapered-thickness, Graphite/epoxy Composite Flywheel,” pp. 1-37, University of California, Laurence Livermore Laboratory, Report No. UCRL-52623 (1978).
2. Analysis of tapered (in steps) laminated plates under uniform inplane load
3. and “Theoretical Investigation of Stress Concentration in Damaged Carbon Fiber Reinforced Plastic Plate Structures,” Progress Report 10, MOD Res. Ag. No. ER/A/9/4/2034/064, Department of Aeronautical Engineering, University of Bristol (1984).
4. The Effect of Geometry on Interlaminar Stresses of [0/90]s Composite Laminates with Circular Holes
5. and “Introduction to Composite Materials,” Technomic Publishing Co., Lancaster, Pennsylvania (1980).