Impact of the fuselage damping characteristics and the blade rigidity on the stability of helicopter

Chellil, AhmedNour, AbdelkaderLecheb, SamirKebir, H.Chevalie, Y.2015-12-132015-12-13201312709638https://dspace.univ-boumerdes.dz/handle/123456789/2529enAerodynamicAeroelasticBladeComposite materialsVibrationDamping characteristicsElastomeric dampersNumerical calculationThree-dimensional modelImpact of the fuselage damping characteristics and the blade rigidity on the stability of helicopterArticle