Condensation of Large Finite-Element Models for Wing Load Analysis with Geometrically-Nonlinear Effects (2013)
Attributed to:
Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Publication URI: http://hdl.handle.net/10044/1/11567
Type: Conference/Paper/Proceeding/Abstract
Parent Publication: Proceedings of the 16th International Forum of Aeroelasticity and Structural Dynamics