Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012)
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.paerosci.2012.06.001
Publication URI: http://dx.doi.org/10.1016/j.paerosci.2012.06.001
Type: Journal Article/Review
Parent Publication: Progress in Aerospace Sciences