The major computational challenge, when using frequency domain linearised computational
fluid dynamics in the analysis of aeroelastic problems such as aircraft flutter, gust response …

The numerical investigation of dynamic responses to atmospheric turbulence is an important
task during the aircraft design and certification process. Efficient methods are desirable …

Several critical load cases during the aircraft design process result from atmospheric
turbulence. Thus, rapidly performable and highly accurate dynamic response simulations …

The major computational challenge, when using frequency domain linearised computational
fluid dynamics in the analysis of aeroelastic problems such as aircraft flutter, gust response …

In this study, an adaptive step size control algorithm incorporated in the continuation method
(CM) is developed and combined with the filtered impulse function method based on …

A quasi-steady doublet-lattice correction method is used to predict aerodynamic gust
responses of two different configurations: a swept wing, the so-called Aerostabil wing, and a …

From 2010 to 2013, several institutes of the German Aerospace Center investigated a
counter rotating fan arrangement called CRISP2. While having efficiency advantages over …

One key task in computational aeroelasticity is to calculate frequency response functions of
aerodynamic coefficients due to structural excitation or external disturbance. Computational …

Predicting loads due to atmospheric turbulence is crucial in the aircraft design and
certification process. Efficient methods are important regarding the large number of …

The flutter behavior of a supercritical airfoil is investigated using a panel formulation, which
solves the subsonic unsteady linearized small-disturbance integral equations. Linear …