ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES

Autor:	Andrei - Daniel VOICU, Anton HADĂR, Daniel VLĂSCEANU
Jazyk:	English<br />French
Rok vydání:	2020
Předmět:	helicopter tail rotor blade laminar composite materials Engineering (General). Civil engineering (General) TA1-2040
Zdroj:	Annals: Series on engineering sciences (Academy of Romanian Scientists), Vol 12, Iss 1, Pp 103-117 (2020)
Druh dokumentu:	article
ISSN:	2066-6950 2066-8570
Popis:	In realizing a high-performance composite material, it is important to take into consideration all the factors that influence the structural response of the component when exposed to service conditions. Thus, in the case of the laminar skin of a composite tail rotor blade, the study of the stress distribution on each lamina is important, so that the optimal design can be chosen. The ACP Post module of the Ansys Workbench finite element software offers the possibility of visualizing the stress distribution on each lamina of the skin, as well as the value of the safety factor for multiple failure criteria.
Databáze:	Directory of Open Access Journals
Externí odkaz:	https://doaj.org/article/9416073dc87d4b689d13c84119ecadd6 Zobrazit plný text záznamu View record in DOAJ