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

dc.contributor.authorChellil, Ahmed
dc.contributor.authorNour, Abdelkader
dc.contributor.authorLecheb, Samir
dc.contributor.authorKebir, H.
dc.contributor.authorChevalie, Y.
dc.date.accessioned2015-12-13T10:40:01Z
dc.date.available2015-12-13T10:40:01Z
dc.date.issued2013
dc.identifier.issn12709638
dc.identifier.urihttps://dspace.univ-boumerdes.dz/handle/123456789/2529
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.relation.ispartofseriesAerospace Science and Technology/ Vol.29, N°1 (2013);pp. 235-252
dc.subjectAerodynamicen_US
dc.subjectAeroelasticen_US
dc.subjectBladeen_US
dc.subjectComposite materialsen_US
dc.subjectVibrationen_US
dc.subjectDamping characteristicsen_US
dc.subjectElastomeric dampersen_US
dc.subjectNumerical calculationen_US
dc.subjectThree-dimensional modelen_US
dc.titleImpact of the fuselage damping characteristics and the blade rigidity on the stability of helicopteren_US
dc.typeArticleen_US

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