Development of Semi-analytical Models for Aircraft Wheel Assembly Design

Author:

Haddar Ahmed,Augustins Louis,Daidie Alain,Rodriguez Emannuel,Diebold Jean-Frédéric

Publisher

Springer Singapore

Reference20 articles.

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2. Schaumann, P.: Global structural behaviour of ring flange joints. In: NAFEMS Seminar , Modelling of Assemblies and Joints for Analyses, 24–25 April 2002, Wiesbaden, Germany (2002)

3. Richtlinien, V.D.I.: VDI 2230. Systematic calculation of highly stressed bolted joints Joints with one cylindrical bolt (2015)

4. Agatonovic, P.: Beam model of beam flanged connections. In: Engineering Computation, vol. 2. Pineridge Press Ltd. (1985)

5. Guillot, J.: Assemblages par éléments filetés: calculs. In: B5560 à B5562, Techniques de l’ingénieur (1987)

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1. Mechanical strength of highly preloaded bolts affected by the ovalization of an aircraft wheel;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2022-01-11

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