Add to ORKGProvably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticit
Graham Ashcroft Institute of Propulsion Technology, German Aerospace Center (DLR), Linder Höhe, 51...
New dissipative time integration algorithms are presented for solving systems of second-order ordina...
A computational method to perform transonic aeroelastic and aeroservoelastic calculations in the tim...
A methodology for designing formally second-order time-accurate and yet loosely-coupled partitioned ...
Abstract: Some numerical aspects for the coupling process of a discrete non-linear aeroelastic syste...
A method is presented for the transient, time domain solution of the structural nonlinear flutter pr...
The extended framework of Hamilton’s principle provides new rigorous weak variational formalism for ...
This paper presents an efficient algorithm for the nonlinear aeroelastic trim analysis of very flexi...
A structural model in the frequency domain is developed to obtain aeroelastic solutions of a NACA64A...
Algorithms for Fluid-Structure Coupling techniques are investigated in the time domain. The accurate...
In this work, a nonlinear state-space-based identification method is proposed to describe compactly ...
The majority of methods for calculating the dynamic response of nonlinear aeroelastic systems consid...
A three-dimensional implicit finite element Euler/Navier-Stokes solver based on the Arbitrary Lagran...
Both linear and nonlinear frequency domain methods have been applied successfully to the investigat...
A novel approach is presented to compute nonlinear aeroelastic trim of highly flexible aircraft by c...
Graham Ashcroft Institute of Propulsion Technology, German Aerospace Center (DLR), Linder Höhe, 51...
New dissipative time integration algorithms are presented for solving systems of second-order ordina...
A computational method to perform transonic aeroelastic and aeroservoelastic calculations in the tim...
A methodology for designing formally second-order time-accurate and yet loosely-coupled partitioned ...
Abstract: Some numerical aspects for the coupling process of a discrete non-linear aeroelastic syste...
A method is presented for the transient, time domain solution of the structural nonlinear flutter pr...
The extended framework of Hamilton’s principle provides new rigorous weak variational formalism for ...
This paper presents an efficient algorithm for the nonlinear aeroelastic trim analysis of very flexi...
A structural model in the frequency domain is developed to obtain aeroelastic solutions of a NACA64A...
Algorithms for Fluid-Structure Coupling techniques are investigated in the time domain. The accurate...
In this work, a nonlinear state-space-based identification method is proposed to describe compactly ...
The majority of methods for calculating the dynamic response of nonlinear aeroelastic systems consid...
A three-dimensional implicit finite element Euler/Navier-Stokes solver based on the Arbitrary Lagran...
Both linear and nonlinear frequency domain methods have been applied successfully to the investigat...
A novel approach is presented to compute nonlinear aeroelastic trim of highly flexible aircraft by c...
Graham Ashcroft Institute of Propulsion Technology, German Aerospace Center (DLR), Linder Höhe, 51...
New dissipative time integration algorithms are presented for solving systems of second-order ordina...
A computational method to perform transonic aeroelastic and aeroservoelastic calculations in the tim...