Abstract
Reliability analysis on the aircraft structures is an integrative study about the structural components and the endured force load on aircraft structures. Especially, the wing reliability is an important index of the aircraft reliability. The reliability of a wing structure model under gust load is analyzed by computer simulation in this paper using the Probability Finite Element Method (PFEM). The gust load, elastic modulus and yield strength are taken as input variables to simulate the reliability problem of the wing structures using the Monte Carlo method, and the influences of the input parameters on aircraft wing strength are obtained. This may provide a viable analysis method for the design and manufacture of an aircraft.
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Ning, X., Yan, Y., Qu, K., Li, Z. (2010). Reliability Analysis on Wing Structures under the Gust Load. In: Wang, F.L., Deng, H., Gao, Y., Lei, J. (eds) Artificial Intelligence and Computational Intelligence. AICI 2010. Lecture Notes in Computer Science(), vol 6320. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-16527-6_5
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DOI: https://doi.org/10.1007/978-3-642-16527-6_5
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-16526-9
Online ISBN: 978-3-642-16527-6
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