1. Kies, J. A., “Maximum Strains in the Resin of Fiberglass Composites,” NRL Report 5752 (March, 1962).
2. Hermann, L. R., and Pister, K. S., “Composite Properties of Filament-Resin Systems,” ASME Paper No. 63-WA-239.
3. Wilson, H. B., and Hill, J. L., “Plane Elastostatic Analysis of an Infinite Plate with a Doubly Periodic Array of Holes or Rigid Inclusions,” in Mathematical Studies of Composite Materials II, Rohm and Haas Co., Report No. S-50, 39 (1965).
4. Foye, R. L., “Structural Composites” North American Aviation, Inc., Columbus Div., Contract No. AF33(615)-5150, Quarterly Reports No. 1, 2, 3, (Sept. 1966, Dec. 1966, March 1967).
5. Adams, D. F., and Doner, D. R., “Transverse Normal Loading of a Unidirectional Composite,” Jnl. Comp. Mats.,1,152–164 (1967). Also, Adams, D. S., Donor, D. R. and Thomas, R. L., “Mechanical Behavior of Fiber Reinforced Composite Materials,” Air Force Materials Lab., AFML-TR-67-96 (1967).