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Estimation of fatigue damage of airplane landing gear

✍ Scribed by Liu, Ke-ge ;Yan, Chu-liang ;Zhang, Shu-ming


Book ID
107378172
Publisher
Higher Education Press and Springer
Year
2006
Tongue
English
Weight
393 KB
Volume
1
Category
Article
ISSN
1673-3479

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This paper analyses the causes of the incident of an F-4 which landed abnormally due to a crack in the nose landing gear hydraulic actuator cylinder. Striations, typical of a fatigue crack, were observed on the fracture surface and a large quantity of corrosive oxide was detected in the initial stag