Full scale aerodynamic wind tunnel testing, numerical simulation of high dimensional (full-
order) aerodynamic models or flight testing are some of the fundamental but complex steps …

This work aims to model transonic airfoil–gust interaction and the gust response on
transonic aileron-buzz problems using high-fidelity computational fluid dynamics (CFD) and …

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

This paper reports an investigation of gust load alleviation using Circulation Control for a
three-dimensional wing including aerodynamic and structure interaction. The Field Velocity …

Predicting gust loads using computational fluid dynamics is prohibitively expensive and
unrealistic for parametric searches. This work presents the development, implementation …

Reduced-order modelling of multidisciplinary computational fluid dynamics can enable
routine industrial gust load analysis. Key to the herein presented model reduction approach …

Shock buffet on wings is a phenomenon caused by strong shock-wave/boundary-layer
interaction resulting first in self-sustained flow unsteadiness and eventually in a detrimental …

The paper presents a methodology for reduced-order modeling of aeroelastic systems
identification and flutter prediction. The aeroelastic system is modeled as a multioutput …

Time domain gust response analysis based on large order nonlinear aeroelastic models is
computationally expensive. An approach to the reduction of nonlinear models for gust …

This paper presents an input–output reduced-order aerodynamic model employing the
kriging interpolation for laminar flow. The kriging interpolation is a regression method …