Abstract
The possibilities to use the M-corrugation type folded aggregates as a part of multilayer panels of the aircraft structures are investigated. A method avoiding complex kinematic calculations for modeling the M-corrugation type folded structure by means of modern computer-aided design systems has been developed and tested. The prospects of developing similar models of the folded structures based on flat-faced corrugations are shown.
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Zakirov, I.M., Alekseev, N.K. & Alekseev, K.A. To the Question of Simplifying the Methodology of Modeling Folded Structures. Russ. Aeronaut. 63, 330–333 (2020). https://doi.org/10.3103/S1068799820020208
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DOI: https://doi.org/10.3103/S1068799820020208