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
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aeroelasticity model for highly flexible aircraft based on the vortex lattice method
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