Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90662/1/AIAA-2011-1917-972.pd
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
This paper investigates the linearization, using perturbation methods, of the structural deformation...
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
A modal solution is presented to the aeroelastic equations of very flexible wings in intrinsic form,...
This paper explores the robust control of large exible wings when their dynamics are written in term...
Dissimilar analysis models are considered for the large structural deformations of aircraft with hig...
A procedure is introduced to construct 1-D geometrically-nonlinear structural dynam- ics models from...
Some classes of aircraft are characterized by highly flexible wings undergoing large structural defo...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77147/1/AIAA-27606-989.pd
The innovative highly flexible wings made of extremely light structures, yet still capable of carryi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76937/1/AIAA-2005-5805-748.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77056/1/AIAA-2006-1636-998.pd
Conventional methodologies for aeroelastic analysis and design are typically based on linear assumpt...
This paper focuses on the characterization of the response of a very flexible aircraft in flight. Th...
This paper investigates the linearization, using perturbation methods, of the structural deformation...
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
This paper investigates the linearization, using perturbation methods, of the structural deformation...
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
A modal solution is presented to the aeroelastic equations of very flexible wings in intrinsic form,...
This paper explores the robust control of large exible wings when their dynamics are written in term...
Dissimilar analysis models are considered for the large structural deformations of aircraft with hig...
A procedure is introduced to construct 1-D geometrically-nonlinear structural dynam- ics models from...
Some classes of aircraft are characterized by highly flexible wings undergoing large structural defo...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77147/1/AIAA-27606-989.pd
The innovative highly flexible wings made of extremely light structures, yet still capable of carryi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76937/1/AIAA-2005-5805-748.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77056/1/AIAA-2006-1636-998.pd
Conventional methodologies for aeroelastic analysis and design are typically based on linear assumpt...
This paper focuses on the characterization of the response of a very flexible aircraft in flight. Th...
This paper investigates the linearization, using perturbation methods, of the structural deformation...
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
This paper investigates the linearization, using perturbation methods, of the structural deformation...
A nonlinear formulation in modal coordinates of the equations of motion of a flexible aircraft is pr...
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