Estimation of the service life of aircraft panel structures under random crack growth rates
Abstract
Keywords
Full Text:
PDF (Українська)References
Goranson, U. G. Damage Tolerance Facts and Fic-tion. International Conference on Damage Tolerance of Aircraft Structures. International Conference on Damage Tolerance of Aircraft Structures, 2007, no. 11. 11 p.
Castro, P. M. S. T., Tavares, S. M. O., Richter-Trummer, V., & Costa, J. D. Damage tolerance of aircraft panels. Mecânica Experimental, 2010, vol. 18, pp. 35-46.
Proppe, C. Probabilistic analysis of multi-site damage in aircraft fuselages. Computational Mechanics, 2003, vol. 30, pp. 323-329. doi: 10.1007/s00466-002-0408-x.
Cavallini, G., & Lazzeri, R. A probabilistic approach to fatigue design of aerospace components by using the risk assessment evaluation. In book: Recent advances in aircraft technology, 2012, pp. 29-48. doi: 10.5772/37784.
Pattabhiraman, S., Kim, N. H., & Haftka, R. T, Effects of uncertainty reduction measures by structural health monitoring on safety and lifecycle cost of airplanes. In: Procedia of 51st Conf. «AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials», 2010, AIAA-2010-2677. doi: 10.2514/6.2010-2677.
Coppe, A., Haftka, R. T., Kim, N. H., & Yuan, F.-G. Uncertainty reduction of damage growth properties using structural health monitoring, Journal of Aircraft, 2010, vol. 47, no. 6, pp. 2030-2038. doi: 10.2514/1.C000279.
Wang, Y., Luo, J., & Daigle, M., Sankararaman, S. Predictive air frame maintenance strategies using model-based prognostics, Journal of Risk and Reliability, 2018, vol. 232, no. 6, pp. 690-709. doi: 10.1177/1748006X18757084.
Giannella, V. On the statistical nature of fatigue crack-growth through Monte Carlo simulations and experimental data, IOP Conference Series: Materials Science and Engineering, 2022, vol. 1214. 8 p. doi: 10.1088/1757-899X/1214/1/012020.
Ciavarella, M., Paggi, M., & Carpinteri, A. One, no one, and one hundred thousand crack propagation laws: A generalized Barenblatt and Botvina dimensional analysis approach to fatigue crack growth, Journal of the Mechanics and Physics of Solids, 2008, vol. 56, no. 12, pp. 3416–3432. doi: 10.1016/j.jmps.2008.09.002.
Ignatovich, S. R., & Karan E. V. Fatigue crack growth kinetics in D16AT aluminum alloy specimens with multiple stress concentrators. Strength of Materials, 2015, vol. 47, no. 4, pp. 586-594. doi: 10.1007/s11223-015-9694-3.
Carpinteri, A., & Paggi, M. Are the Paris’ law parameters dependent on each other? Frattura ed Integrità Strutturale, 2007, vol. 2, no. 2, pp. 10-16. doi: 10.3221/IGF-ESIS.02.02.
Ihnatovych, S. R., Karuskevych, M. V., Yutskevych, S. S., Karan, Ye. V., & Dzhavadova, I. I. Prohnozuvannya zalyshkovoyi dovhovichnosti konstruktsiy z alyuminiyevykh splaviv pry vypadkoviy shvydkosti zrostannya vtomnykh trishchyn [Prediction of residual fatigue life of aluminum alloy structures under random fatigue crack growth rate]. Problemy mitsnosti - Strength of Materials, 2025, vol. 1, pp. 52–64. (in Ukrainian).
Baker, M., & Stanley, I. Assessing and modelling the uncertainty in fatigue crack growth in structural steels, HSE Research Report RR643, 2008. 99 p.
Sinclair, G. B., & Pierie, R. V. On obtaining fatigue crack growth parameters from the literature, International Journal of Fatigue, 1990, vol. 12, no. 1, pp. 57-62. doi: 10.1016/0142-1123(90)90343-D.
Bergner, F., & Zouhar, G. A new approach to the correlation between the coefficient and the exponent in the power law equation of fatigue crack growth, International Journal of Fatigue, 2000, vol. 22, no. 3, pp. 229-239. doi: 10.1016/S0142-1123(99)00123-1.
Coppe, A., Pais, M. J., Haftka, R. T., & Kim, N. H. Using a simple crack growth model in predicting remaining useful life, Journal of Aircraft, 2012, vol. 49, no. 6, pp. 1965-1973. doi: 10.2514/1.C031808.
Dzhavadova, I. Metody vyznachennya koefitsiyentiv intensyvnosti napruzhen' u aviatsiynykh konstruktsiyakh [Stress intensity factor determination methods for aircraft structures]. Aviatsiyno-kosmichna tekhnika i tekhnolohiya - Aerospace technic and technology, 2024, vol. 4 (196), pp. 24–33. doi: 10.32620/aktt.2024.4.03. (in Ukrainian).
DOI: https://doi.org/10.32620/aktt.2025.4sup2.07