PSI - Issue 24

Filippo Cianetti et al. / Procedia Structural Integrity 24 (2019) 526–540 Author name / Structural Integrity Procedia 00 (2019) 000–000

540

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http://dx.doi.org/10.1016/j.proeng.2014.09.111 , doi: 10.1016/j.proeng.2014.09.111 . Ru˚zˇek, R., Beˇhal, J., 2009. Certification programme of airframe primary structure composite part with environmental simulation. International Journal of Fatigue 31, 1073–1080. doi: 10.1016/j.ijfatigue.2008.05.028 . Schijve, J., 1994. Fatigue of aircraft materials and structures. International Journal of Fatigue 16, 21–32. doi: 10.1016/0142-1123(94)90442-1 . Xu, H., Liu, D., Xue, Y., Zhou, L., Min, G., 2012. Airworthiness compliance verification method based on simulation of complex system. Chinese Journal of Aeronautics 25, 681–690. URL: http://dx.doi.org/10.1016/S1000-9361(11)60434-2 , doi: 10.1016/S1000-9361(11) 60434-2 . Zaman, I., Khalid, A., Manshoor, B., Araby, S., Ghazali, M.I., 2013. The e ff ects of bolted joints on dynamic response of structures. IOP Conference Series: Materials Science and Engineering 50. doi: 10.1088/1757-899X/50/1/012018 . Zucca, G., Cianetti, F., Palmieri, M., Braccesi, C., Paolis, F.D., De Paolis, F., 2018. Fatigue Life Extimation of a Military Aircraft Structure subjected to Random Loads. Procedia Structural Integrity 12, 183–195. URL: https://linkinghub.elsevier.com/retrieve/pii/ S2452321618301999 , doi: 10.1016/j.prostr.2018.11.096 .

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