In this work, a new approach for the generation of a generalized state-space
aeroservoelastic model based on tangential interpolation is presented. The resulting system …

The steady and unsteady aerodynamic predictions of the Doublet Lattice Method (DLM) are
routinely corrected for camber, twist, and transonic effects using steady reference data …

A transonic aeroelastic optimization approach for composite wing structure is proposed in
this study. Aerodynamic influence coefficient matrices are generated using doublet lattice …

The steady and unsteady aerodynamic predictions of the Doublet Lattice Method (DLM) are
routinely corrected for camber, twist, dihedral and transonic effects using steady reference …

A simplified method for gust modeling in CFD simulations, the so-called Disturbance
Velocity Approach (DVA), is analyzed within this work. This approach covers the influence of …

This study proposes a design procedure for the multi-objective aeroelastic optimization of a
tow-steered composite wing structure that operates at transonic speed. The aerodynamic …

To date, there is limited knowledge on the topic of unsteady nonlinear transonic flow caused
by large-amplitude excitations. The Certification Specifications for Large Aeroplanes …

Large-amplitude excitations need to be considered for gust load analyses of transport
aircraft in cruise flight conditions. Nonlinear amplitude effects in transonic flow are, however …

Practical gust loads analysis involves computationally expensive parameter studies. In
particular, the gust amplitude varies with gust length as defined by regulatory bodies …

In this paper the multi-disciplinary simulation of unsteady flight maneuvers is carried out
using reduced-order models (ROM) based on Reynolds Averaged Navier-Stokes (RANS) …