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- W2001797189 abstract "Aircraft MLG and wing structures have been recognized as fatigue critical structures and exposed to the risk of fatigue crack initiation and propagation. Furthermore, these structures are frequently subjected to serious dynamic loading condition during a Hard Landing which may lead to their failure. Especially, structural integrity of MLG and wing components is decreased as the flight time increased because of the fatigue damage accumulated on the aircraft. In this study, the effects of Hard Landing on the MLG and wing components of aging aircraft were evaluated by using numerical approach. To achieve the aim, a finite element model has been developed and simulations were conducted by varying the landing conditions. As a result, it was revealed that the high stress concentration phenomenon was occurred at the lower Side Brace of MLG. Thereby, the intensified inspection for the lower Side Brace should be considered to prevent unexpected aircraft mishap." @default.
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- W2001797189 date "2011-10-05" @default.
- W2001797189 modified "2023-09-24" @default.
- W2001797189 title "A Study of the Effects of Hard Landing on Aircraft Structure" @default.
- W2001797189 doi "https://doi.org/10.9766/kimst.2011.14.5.805" @default.
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