EVOLUTIONARY MODEL OF FATIGUE FRACTURE UNDER IRREGULAR LOADING

Author:

Petukhov D. S.,Keller I. E.

Publisher

Allerton Press

Subject

General Physics and Astronomy,Mechanics of Materials

Reference15 articles.

1. V. E. Strizhius, Calculation Methods for Fatigue Endurance of Aero-Construction Elements (Mashinostroenie, Moscow, 2012) [in Russian].

2. A. Z. Vorobyov, B. I. Olkin, V. N. Stebenev, and T. S. Rodchenko, Resistance Fatigue of Structural Elements (Mashinostroenie, Moscow, 1990) [in Russian].

3. H. F. S. G. Pereira, D. L. DuQuesnay, A. M. P. De Jesus, A. L. L. Silva, “Analysis of variable amplitude fatigue data of the P355NL1 steel using the effective strain damage model,” ASME J. Pressure Vessel Technol. 131 (5), 051402 (2009). https://doi.org/10.1115/1.3147986

4. W. Schütz and P. Heuler, “Miner’s rule revisited,” in AGARD Report, No. 797: An Assessment of Fatigue Damage and Crack Growth Prediction Techniques (AGARD, 1994), P. 1.1.

5. J. C. Ekvall and L. Young, “Converting fatigue loading spectra for flight-by-flight testing of aircraft and helicopter components,” J. Test. Eval. 4 (4), 231–247 (1976). https://doi.org/10.1520/JTE10207J

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