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.
To the Question of Simplifying the Methodology of Modeling Folded Structures
Russ. Aeronaut.
Russian Aeronautics ; 63 , 2 ; 330-333
2020-04-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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