“…The material and mechanical properties relevant to strain life curves used to determine the observed landing gear leg RUL made from a 6150 steel alloy, also referred to as the 51CrV4 steel alloy, were determined through rigorous literature research. This involved a review of academic journals, industry publications, and technical reports [27][28][29][30][31][32][33][34], leading to the identification of key material fatigue-relevant properties. The properties of this alloy include a density of 7850 kg/m 3 , Young's modulus of 2.038 × 10 11 Pa, Poisson's ratio of 0.29, strength coefficient of 1.1 × 10 9 Pa, strength exponent of −0.093, ductility coefficient of 0.478, ductility exponent of −0.684, cyclic strength coefficient of 1.476 × 10 9 Pa, cyclic strain hardening exponent of 0.0651, tensile and compressive yield strength of 1.042 × 10 9 Pa, and tensile ultimate strength of 1.2773 × 10 9 Pa. Program-controlled element order and adaptive element sizing, with a maximum element size of 1.4 × 10 −2 m, have culminated in an acceptable RUL regarding prediction expectancy based on the recorded number of airplane landings in the airplane technical logbook.…”