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 …

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 …

The aim of this article is to investigate the parameter sensitivity of the (Non-Linear) Unsteady
Vortex Lattice Method-Vortex Particle Method [(NL-) UVLM-VPM] with Particle Strength …

The present investigation addresses two key issues in aerodynamic performance of a
propeller–wing configuration, namely linear and nonlinear predictions with low-order …

基于2.5 D RANS 数据和VLM 耦合的方式, 发展了一种考虑非线性流动效应的混合型涡格法
HVLM. 采用矩形直/后掠机翼两个外形的跨声速算例, 通过与VLM, 三维CFD 计算数据的比较 …

The design process of transonic civil aircraft is complex and requires strong governance to
manage the various program development phases. There is a need in the community to …

The flight envelope of civil aircraft is bounded by several complex aerodynamic phenomena,
of those the stall and the buffeting of lifting surfaces. Stall is defined as a loss of lift caused by …

H and smaller lifting rotor (s) unmanned aerial vehicles (UAVs) remain unequaled for
missions in confined environment such as close to cliffs, buildings or aircraft carriers …

Calculating the unsteady convective heat transfer on helicopter blades is a first step in the
prediction of ice accretion and the design of ice-protection systems. CFD simulations are …