Publisher
Springer Berlin Heidelberg
Reference8 articles.
1. Newman, J. C., Jr., “A Crack Closure Model for Predicting Fatigue Crack Growth Under Aircraft Spectrum Loading,” Methods and Models for Predicting Fatigue Crack Growth Under Random Loading. ASTM STP 748, American Society for Testing and Material, 1981, pp. 53-84.
2. Phillips, E. P. and Newman, J. C., Jr., “Impact of Small-crack Effects on Design-Life Calculations,” Experimental Mechanics. Vol 29, No 2, June 1989, pp. 221–225.
3. Tan, P. W., Raju, I. S. and Newman, J. C., Jr., “Boundary Force Method for Analyzing Two-Dimensional Cracked Bodies,” NASA TM-87725, May 1986.
4. Shivakumar, K. N., Tan, P. W. and Newman, J. C., Jr., “A Virtual Crack-Closure Technique for Calculating stress Intensity Factors for Cracked Three Dimensional Bodies,” International Journal of Fracture. Vol. 36, 1988, pp. R43–R50.
5. Dawicke, D. S.; Poe, C. C., Jr.; Newman, J. C., Jr.; and Harris, C. E.; “An Evaluation of the Pressure Proof Test Concept for Thin Sheet 2024-T3,” NASA TM-101675, 1990.
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