1. Durelli, A. J., Lake, R. L., andTsao, C. H., “Device for Applying Uniform Loading to Boundaries of Complicated Shape,” Proc. SESA, XI,No. 1, 55–61 (1953).
2. Barriage, J. B., andDurelli, A. J., “Application of a New Deformeter to Two-Dimensional Thermal Stress Problems,”Ibid., XIII,No. 2, 97–106 (1956).
3. Durelli, A. J., and Hofer, K., “Photoelastic Studies of Stress and Strain Concentration Factors Associated with Rocket Propellant Grain Designs,” Final Report, Armour Research Foundation, Project No, K165, Phase I, April 1959, to Thiokol Chemical Corp., Elkton Division, Elkton, Md.
4. Durelli, A. J., and Daniel, I. M., “Optimization of Outer Contour of Rocket Propellant Grain Designs,” Final Report, Armour Research Foundation, Project No. K165, Phase 2, June 1959, to Thiokol Chemical Corp., Elkton Division, Elkton, Md.
5. Durelli, A. J., and Lake, R. L., “Determination of Optinum Geometry for Star-Perforated Propellant Grains,” Final Report, Armour Research Foundation, Project K036-7, February 1953, to Thiokol Chemical Corp., Huntsville, Ala.