Nonlinear Aeroelasticity of Highly Flexible Joined-Wing Aircraft using Unsteady Vortex-Lattice Method
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2017-01-01
Conference paper
Electronic Resource
English
Exploratory Studies of Joined-Wing Aeroelasticity
AIAA | 2005
|Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
Online Contents | 2012
|Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
British Library Conference Proceedings | 2009
|