Radial basis functions mesh morphing: A comparison between the bi-harmonic spline and the wendland c2 radial function

ME Biancolini, A Chiappa, U Cella, E Costa… - International Conference …, 2020 - Springer
Radial basis functions (RBFs) based mesh morphing allows to adapt the shape of a
computational grid onto a new one by updating the position of all its nodes. Usually nodes …

Upscaling 2D finite element analysis stress results using radial basis functions

A Chiappa, P Salvini, C Brutti, ME Biancolini - Computers & Structures, 2019 - Elsevier
This paper presents a method of interpolation and regularisation of finite element (FE)
results based on radial basis functions (RBF) capable to upscale at a finer resolution the …

Wind tunnel model design and aeroelastic measurements of the ribes wing

U Cella, P Della Vecchia, C Groth… - Journal of Aerospace …, 2021 - ascelibrary.org
Several experimental databases of aeroelastic measurements performed on aircraft wing
models are available for the validation of fluid–structure interaction (FSI) numerical …

Testing and evaluation of the structural performance of a 3D-printed polylactic acid aircraft wing rib

R Dogea, XT Yan, R Millar - Discover Mechanical Engineering, 2023 - Springer
This paper presents an investigation of the structural performance of a 3D-printed Polylactic
Acid (PLA) wing rib structure that is integrated with Internet of Things (IoT) sensory …

Validation of structural modeling for realistic wing topologies involved in fsi analyses: Ribes test case

ME Biancolini, C Groth, S Porziani… - Journal of Aerospace …, 2021 - ascelibrary.org
The procedures that couple finite-element method (FEM) solutions and fluid dynamic solvers
to develop so-called high-fidelity fluid–structure interaction (FSI) numerical methods involve …

[图书][B] Flexible Engineering Toward Green Aircraft

ME Biancolini, U Cella - 2020 - Springer
Modern engineering design and analysis tools very often involve shape modifications for
which an opportune geometric parametrization strategy is required. The efficiency of the …

Motorlu çok hafif hava aracının prototipinin tasarımı ve geliştirilmesi

K Özpınar - 2022 - search.proquest.com
Bu çalışmada motorlu çok hafif hava aracının tasarımı ve analizleri yapılmıştır. Uçak tasarımı,
kavramsal tasarım, ön tasarım, detaylı tasarım ve analiz bölümlerine bölünerek incelenmiştir …

[PDF][PDF] Discover Mechanical Engineering

R Dogea, XT Yan, R Millar - Discover, 2023 - core.ac.uk
This paper presents an investigation of the structural performance of a 3D-printed Polylactic
Acid (PLA) wing rib structure that is integrated with Internet of Things (IoT) sensory …

Aeroelastic wind tunnel tests of the RIBES wing model

F Nicolosi, V Cusati, D Ciliberti, P Della Vecchia… - … Toward Green Aircraft …, 2020 - Springer
Aeroelastic wind tunnel tests on a half-wing model have been performed at the University of
Naples “Federico II” to acquire data about aerodynamic forces, section pressure coefficient …