1. Damage Tolerance in Aircraft Structures;Elber;ASTM STP,1971
2. Gerber, T. L. (1970). The Effect of Tensile Preload on the Fatigue Strength of Notched Steel Bars. ASTM STP 467. p. 276. Americam Society for Testing and Materials.
3. Lin, Li., Y. Tao and N. S. Hu (1988). A Reformed Model for Fatigue Crack Growth with Residual Stress Field. In: Proc. of 2nd Inter. Conf. on Residual Stresses (G. Beck., S. Denis and A. Simon eds.). Elsevier Applied Science. Oxford, pp. 815–819.
4. Fatigue Crack Growth Retardation after Single- Cyclic Overload in Ti-6A1–4V Titanium Alloy;Jones;Engng Fract. Mech.,1973
5. Macroscopic Residual Stress Distribution at a Fatigue Crack Tip;Kunz;Fatigue Engng Mater. & Struct.,1979