For decades panel methods have been used in the industrial context to compute the unsteady aerodynamic model for gust load purposes. Additionally corrections with wind tunnel and/or steady CFD data have been applied to overcome the shortcomings of the panel methods, especially in the transonic regime. With the aim to compute a more realistic unsteady aerodynamic model without corrections, computational fluid dynamics (CFD) should replace the panel methods in the future. Due to the large computational costs of CFD, an important enabler for the direct usage of unsteady CFD in the industrial context is linearized CFD. These codes allow computing harmonic motion and harmonic gusts directly in the frequency domain, preventing expansive unstead...
Gust analysis is one key task during design and certification of new aircraft. In the industrial sta...
Aeroelastic stability must be maintained for the entire flight duration. Of the vast phenomena that ...
The increased flexibility of long endurance aircraft having high aspect ratio wings necessitates att...
This paper provides an overview about the time-linearized analysis of motion-induced and gust-induce...
The numerical investigation of dynamic responses to atmospheric turbulence is an important task duri...
Gust load alleviation has become an integral part of aircraft design to significantly decrease the i...
In this paper the multi-disciplinary simulation of unsteady flight maneuvers is carried out using re...
A tremendous number of gust load cases needs to be computed during the aircraft design and certifica...
This paper presents a novel approach to computing aircraft total loads generated by a gust encounte...
Two different methods for modeling of gusts have been implemented into the CFD-code TAU. The first o...
Computational engineering methods play a more and more important role in building aircraft that move...
This work gives an overview of the nonlinear reduced order modeling (ROM) approach for unsteady aero...
Gust load analysis is a relevant part of the certification process of aircraft. In need of low compu...
Two different methods for modeling of atmospheric effects have been implemented into the CFD code TA...
ABSTRACTSeveral critical load cases during the aircraft design process result from atmospheric turbu...
Gust analysis is one key task during design and certification of new aircraft. In the industrial sta...
Aeroelastic stability must be maintained for the entire flight duration. Of the vast phenomena that ...
The increased flexibility of long endurance aircraft having high aspect ratio wings necessitates att...
This paper provides an overview about the time-linearized analysis of motion-induced and gust-induce...
The numerical investigation of dynamic responses to atmospheric turbulence is an important task duri...
Gust load alleviation has become an integral part of aircraft design to significantly decrease the i...
In this paper the multi-disciplinary simulation of unsteady flight maneuvers is carried out using re...
A tremendous number of gust load cases needs to be computed during the aircraft design and certifica...
This paper presents a novel approach to computing aircraft total loads generated by a gust encounte...
Two different methods for modeling of gusts have been implemented into the CFD-code TAU. The first o...
Computational engineering methods play a more and more important role in building aircraft that move...
This work gives an overview of the nonlinear reduced order modeling (ROM) approach for unsteady aero...
Gust load analysis is a relevant part of the certification process of aircraft. In need of low compu...
Two different methods for modeling of atmospheric effects have been implemented into the CFD code TA...
ABSTRACTSeveral critical load cases during the aircraft design process result from atmospheric turbu...
Gust analysis is one key task during design and certification of new aircraft. In the industrial sta...
Aeroelastic stability must be maintained for the entire flight duration. Of the vast phenomena that ...
The increased flexibility of long endurance aircraft having high aspect ratio wings necessitates att...