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:
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