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- W2386352409 abstract "Design of flutter model from aircraft metal structure to composite structure can be achieved by equation of stiffness, yet it may cost much time for general design method. A design method based on design element for finite element model of aircraft structure is proposed in this paper. First the finite element model is discreted further, then the design process can be finished based on equation of stiffness and with engineer design-produce as constrain condition. Combining experiment results, the feasibility and rationality of the design method are validated." @default.
- W2386352409 created "2016-06-24" @default.
- W2386352409 creator A5021440074 @default.
- W2386352409 date "2006-01-01" @default.
- W2386352409 modified "2023-09-25" @default.
- W2386352409 title "Design of Low-Velocity Wing Tunnel Flutter Model of Aircraft Composite Structure" @default.
- W2386352409 hasPublicationYear "2006" @default.
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