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

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

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...

Full description

Bibliographic Details
Main Authors: Andrei - Daniel VOICU, Anton HADĂR, Daniel VLĂSCEANU
Format: Article
Language:English
Published: Editura Academiei Oamenilor de Știință din România 2020-08-01
Series:Annals: Series on engineering sciences (Academy of Romanian Scientists)
Subjects:
helicopter tail rotor blade
laminar composite materials
Online Access:http://aos.ro/wp-content/anale/TVol12Nr1Art.8.pdf
id doaj-9416073dc87d4b689d13c84119ecadd6
record_format Article
spelling doaj-9416073dc87d4b689d13c84119ecadd62020-11-25T03:34:41Zeng Editura Academiei Oamenilor de Știință din România Annals: Series on engineering sciences (Academy of Romanian Scientists)2066-69502066-85702020-08-01121103117ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCESAndrei - Daniel VOICU0Anton HADĂR1Daniel VLĂSCEANU2University Politehnica of Bucharest, RomaniaAcademy of Romanian Scientists, University POLITEHNICA of Bucharest, RomaniaUniversity Politehnica of Bucharest, Romania 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.http://aos.ro/wp-content/anale/TVol12Nr1Art.8.pdfhelicopter tail rotor bladelaminar composite materials
collection DOAJ
language English
format Article
sources DOAJ
author Andrei - Daniel VOICU
Anton HADĂR
Daniel VLĂSCEANU
spellingShingle Andrei - Daniel VOICU
Anton HADĂR
Daniel VLĂSCEANU
ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
Annals: Series on engineering sciences (Academy of Romanian Scientists)
helicopter tail rotor blade
laminar composite materials
author_facet Andrei - Daniel VOICU
Anton HADĂR
Daniel VLĂSCEANU
author_sort Andrei - Daniel VOICU
title ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
title_short ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
title_full ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
title_fullStr ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
title_full_unstemmed ASPECTS REGARDING INTERLAMINAR STRESS DISTRIBUTION ON THE COMPOSITE LAMINATED SKIN OF A TAIL ROTOR BLADE EXPOSED TO AERODYNAMIC FORCES
title_sort aspects regarding interlaminar stress distribution on the composite laminated skin of a tail rotor blade exposed to aerodynamic forces
publisher Editura Academiei Oamenilor de Știință din România
series Annals: Series on engineering sciences (Academy of Romanian Scientists)
issn 2066-6950
2066-8570
publishDate 2020-08-01
description 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.
topic helicopter tail rotor blade
laminar composite materials
url http://aos.ro/wp-content/anale/TVol12Nr1Art.8.pdf
work_keys_str_mv AT andreidanielvoicu aspectsregardinginterlaminarstressdistributiononthecompositelaminatedskinofatailrotorbladeexposedtoaerodynamicforces
AT antonhadar aspectsregardinginterlaminarstressdistributiononthecompositelaminatedskinofatailrotorbladeexposedtoaerodynamicforces
AT danielvlasceanu aspectsregardinginterlaminarstressdistributiononthecompositelaminatedskinofatailrotorbladeexposedtoaerodynamicforces
_version_ 1724558160158523392

Similar Items