In this paper, we present an aero‐structural model of a tethered swept wing for airborne
wind energy generation. The carbon composite wing has neither fuselage nor actuated …

T design of high-lift (HL) systems represents an important and complex task for transport
aircraft designers and has gained importance over the last decades. HL devices have a …

This study presents a hybrid non-linear unsteady vortex lattice method-vortex particle
method (NL UVLM-VPM) to investigate the aerodynamics of rotor blades hovering in and out …

Abstract The Unsteady Vortex Lattice Method has interesting capabilities for nonlinear
subsonic aeroelastic analyses. This paper aims to develop an aeroelastic framework based …

Aircraft morphing provides advantages to traditional flight including drag reduction and
maneuverability. Previous research indicates that smooth spanwise transitions in trailing …

The paper presents a numerical framework for the aerodynamic analysis of aircraft wings in
transonic cruise and take-off/landing compatible with preliminary and conceptual design …

View Video Presentation: https://doi. org/10.2514/6.2022-4149. vid The performance-
improvement objectives sought in future commercial aircraft may require a significant …

With the increase in icing constraints imposed by the aircraft certification authorities, it is
becoming more important to consider ice accumulation early in the aircraft design studies …

T e conceptual aerodynamic design of wings is a phase that requires a balance between
cost and accuracy: the aerodynamic tools used must provide reliable results relatively fast so …

Résumé Les simulations numériques prennent de plus en plus de place dans les processus
de conception et de certification en ingénierie, il en va de même dans le domaine de …