Nonlinear Aeroelasticity of Highly Flexible Joined-Wing Aircraft using Unsteady Vortex-Lattice Method
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Exploratory Studies of Joined-Wing Aeroelasticity
AIAA | 2005
|Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
Online Contents | 2012
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