1. AGMA Standard, 1983, “Practice for Carburized Aerospace Gearing”,American Gear Manufacturers Association, 246.02A. pp. 11–14.
2. Ahmad, J. and Loo F. T., 1977, “On the Use of Strain Energy Density Fracture Criterion in the Design of Grears Using Finite Element Method”,ASME 77-DET-158, pp. 1–8.
3. Besuner, P. M., 1876. “Residual Life Estimates for Structures with Partial Thickness Cracks”. Mechanics of Crack Growth,ASTM STP 590, American Society for Testing and Materials, pp. 403–419.
4. Honda, H. and Conway, J. C., “An Analysis by Finite Element Techniques of the Effects of a Crack in the Gear Tooth Fillet and Its Applicability to Evaluating Strength of the Flawed Grears”,Bull. JSME, Vol. 22, 1979, pp. 1848–1855.
5. Inoue, K., Kato, M., and Yamanaka, M. 1989, “Fatigue Strength and Crack Growth of Carburized and Shot Peened Spur Grears”,Journal of ASME, Book No. 10288B, pp. 663–668.