Residual-stress effects at a notch root in A723 steel to extend fatigue life

Author:

Underwood John H.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference8 articles.

1. Underwood, J.H. and Throop, J.F., “Residual Stress Effects on Fatigue Cracking of Pressurized Cylinders and Notched Bending Specimens,” Proc. 1980 SESA Spring Meeting, (May 1980).

2. Wohlfahrt, H., “Shot Peening and Residual Stress,” Residual Stress and Stress Relaxation, eds. E. Kula and V. Weiss, Plenum, 71–92 (1982).

3. Loomis, K., unpublished results, Army Armament RD&E Center, Watervliet, NY.

4. Underwood, J.H. and Kapp, J.A., “Benefits of Overload for Fatigue Cracking at a Notch,” Fracture Mechanics: Thirteenth Conference, ASTM STP 743, ed. R. Roberts, Amer. Soc. Test, and Mat., 48–62 (1982).

5. Underwood, J.H. and Throop, J.F., “Surface Crack K Estimates and Fatigue Life Calculations in Cannon Tubes,” Part-Through Crack Fatigue Life Prediction, ASTM STP 687, ed. J.B. Chang, Amer. Soc. Test. and Mat., 195–210 (1979).

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