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