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• W2313247949 abstract "A finite element based stability analysis is developed for a hingeless, composite, isolated rotor in hover. It includes a mechanism for the inclusion of a complete 6 x 6 stiffness matrix, as well as the effects of rotary inertia. No restrictions are made on the magnitudes of the displacements and rotations if the magnitudes of the strains remain small compared to unity. The equilibrium position is obtained by an iterative solution of the complete nonlinear equations. The dynamic equations are linearized about this position, yielding and eigenproblem. The lift model is a two-dimensional, quasi-steady strip theory, with inflow taken from momentum theory. Initial results are given for the stability of extensiontwist coupled rotor blades." @default.
• W2313247949 created "2016-06-24" @default.
• W2313247949 creator A5013484052 @default.
• W2313247949 creator A5020992691 @default.
• W2313247949 date "1992-04-13" @default.
• W2313247949 modified "2023-09-26" @default.
• W2313247949 title "Application of composite rotor blade stability analysis to extension-twist coupled blades" @default.
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• W2313247949 doi "https://doi.org/10.2514/6.1992-2254" @default.
• W2313247949 hasPublicationYear "1992" @default.
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