Calibration of crack growth model for damage tolerance analysis

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Journal of the Korea Institute of Military Science and Technology 2002;5(4):67-77.

¹
²

손상허용해석을 위한 균열성장모델 교정

주영식, 김재훈

¹국방과학연구소
²충남대학교 기계설계공학과

Abstract

This paper introduces the calibration results of the fatigue crack growth models for damage tolerance analysis of the aircraft structures. Generalized Willenborg model and Wheeler model are calibrated with experimental data tested under the load spectrum of a trainer. The retardation factors such as, shut-off ratio in Generalized Willenborg model and shaping exponent in Wheeler model, are evaluated for aluminum alloys AL2024-T3511, AL7050-T7451 and AL7075-T73511. It is shown that the retardation effect of the crack growth rate depends on the yield strength of material and the maximum stress in the load spectrum. Generalized Willenborg model and Wheeler model give satisfactory prediction of crack growth life but the calibration of the experimental parameters with test is required.

Key Words: Damage tolerance, Durability, Crack growth retardation, Crack growth rate, Overload, Load spectrum