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A method for normal-mode-based model reduction in nonlinear dynamics of slender structures (2015)

First Author: Wang Y

Attributed to: Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.compstruc.2015.07.001

Publication URI: http://dx.doi.org/10.1016/j.compstruc.2015.07.001

Type: Journal Article/Review

Parent Publication: Computers & Structures