STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE

STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE

—The aerospace industry deals from the beginning with structures with special requirements as extreme lightweight and withstanding to a big number of load cases. Aerodynamics constraints lead to supplementary restrictions, the results being the complex shape to sustain the fuselage, the rotor blades...

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Bibliographic Details
Main Authors: CAZANGIU Diana, DIMA Gabriel, DRAGAN Razvan, ROSCA Ileana
Format: Article
Language:English
Published: Editura Universităţii din Oradea 2014-05-01
Series:Annals of the Oradea University: Fascicle Management and Technological Engineering
Subjects:
Keywords:finiteelementmethod
hoveringflightmode
rotorblade
structuralanalysis
Online Access:http://imtuoradea.ro/auo.fmte/files-2014-v1/Cazangiu Diana-STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE.pdf
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spelling doaj-0d50943532a24e39868075515a37b5492020-11-24T21:43:27ZengEditura Universităţii din OradeaAnnals of the Oradea University: Fascicle Management and Technological Engineering1583-06911583-06912014-05-01XXIII (XIII)10.AUOFMTE.2014-1.29642964STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODECAZANGIU DianaDIMA GabrielDRAGAN RazvanROSCA Ileana—The aerospace industry deals from the beginning with structures with special requirements as extreme lightweight and withstanding to a big number of load cases. Aerodynamics constraints lead to supplementary restrictions, the results being the complex shape to sustain the fuselage, the rotor blades or the wings skin. This paper presents a static structural analysis of the main rotor blade for the light helicopter. To simulate the mechanical behavior of the blade, a finite elements method was used. A case of hovering flight mode was considered.http://imtuoradea.ro/auo.fmte/files-2014-v1/Cazangiu Diana-STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE.pdfKeywords:finiteelementmethodhoveringflightmoderotorbladestructuralanalysis
collection DOAJ
language English
format Article
sources DOAJ
author CAZANGIU Diana
DIMA Gabriel
DRAGAN Razvan
ROSCA Ileana
spellingShingle CAZANGIU Diana
DIMA Gabriel
DRAGAN Razvan
ROSCA Ileana
STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
Annals of the Oradea University: Fascicle Management and Technological Engineering
Keywords:finiteelementmethod
hoveringflightmode
rotorblade
structuralanalysis
author_facet CAZANGIU Diana
DIMA Gabriel
DRAGAN Razvan
ROSCA Ileana
author_sort CAZANGIU Diana
title STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
title_short STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
title_full STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
title_fullStr STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
title_full_unstemmed STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE
title_sort structural analysis of the main rotor blade for a light helicopter - case of hovering flight mode
publisher Editura Universităţii din Oradea
series Annals of the Oradea University: Fascicle Management and Technological Engineering
issn 1583-0691
1583-0691
publishDate 2014-05-01
description —The aerospace industry deals from the beginning with structures with special requirements as extreme lightweight and withstanding to a big number of load cases. Aerodynamics constraints lead to supplementary restrictions, the results being the complex shape to sustain the fuselage, the rotor blades or the wings skin. This paper presents a static structural analysis of the main rotor blade for the light helicopter. To simulate the mechanical behavior of the blade, a finite elements method was used. A case of hovering flight mode was considered.
topic Keywords:finiteelementmethod
hoveringflightmode
rotorblade
structuralanalysis
url http://imtuoradea.ro/auo.fmte/files-2014-v1/Cazangiu Diana-STRUCTURAL ANALYSIS OF THE MAIN ROTOR BLADE FOR A LIGHT HELICOPTER - CASE OF HOVERING FLIGHT MODE.pdf
work_keys_str_mv AT cazangiudiana structuralanalysisofthemainrotorbladeforalighthelicoptercaseofhoveringflightmode
AT dimagabriel structuralanalysisofthemainrotorbladeforalighthelicoptercaseofhoveringflightmode
AT draganrazvan structuralanalysisofthemainrotorbladeforalighthelicoptercaseofhoveringflightmode
AT roscaileana structuralanalysisofthemainrotorbladeforalighthelicoptercaseofhoveringflightmode
_version_ 1725914123950096384

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