[HTML][HTML] UCNS3D: An open-source high-order finite-volume unstructured CFD solver

AF Antoniadis, D Drikakis, PS Farmakis, L Fu… - Computer Physics …, 2022 - Elsevier
UCNS3D is an open-source computational solver for compressible flows on unstructured
meshes. State-of-the-art high-order methods and their associated benefits can now be …

Review of rotating wing dynamic stall: Experiments and flow control

AD Gardner, AR Jones, K Mulleners… - Progress in Aerospace …, 2023 - Elsevier
Dynamic stall has been a technical challenge and a fluid dynamical subject of interest for
more than fifty years; but in the last decade significant advances have been made in the …

[HTML][HTML] Simple multiple reference frame for high-order solution of hovering rotors with and without ground effect

PASF Silva, P Tsoutsanis, AF Antoniadis - Aerospace Science and …, 2021 - Elsevier
In the present work, the aerodynamic performance of the Caradonna and Tung and S-76 in
hover were investigated using a simplified concept of multiple reference frame (MRF) …

Wakes of rotorcraft in advancing flight: A large-eddy simulation study

DG Caprace, P Chatelain, G Winckelmans - Physics of Fluids, 2020 - pubs.aip.org
We perform the large-eddy simulation of the flow past a helicopter rotor to support the
investigation of rotorcraft wake characteristics and decay mechanisms. A hybrid Lagrangian …

Meta‐Lens Particle Image Velocimetry

X Liu, Z Zhao, S Xu, J Zhang, Y Zhou, Y He… - Advanced …, 2024 - Wiley Online Library
Fluid flow behavior is visualized through particle image velocimetry (PIV) for understanding
and studying experimental fluid dynamics. However, traditional PIV methods require multiple …

A robust method for reliable transition detection in temperature-sensitive paint data

M Costantini, U Henne, S Risius, C Klein - Aerospace Science and …, 2021 - Elsevier
This work presents a method to automatically detect boundary-layer transition on
thermographic images of aerodynamic surfaces, acquired using the temperature-sensitive …

DES of a Slingsby Firefly aircraft: Unsteady flow feature extraction using POD and HODMD

A Corrochano, AF Neves, B Khanal… - Journal of Aerospace …, 2022 - ascelibrary.org
In this paper, higher-order dynamic mode decomposition (HODMD) was applied to find the
main patterns and frequencies of a transient aerodynamic flow field when an aircraft wing …

Wall-resolved large eddy simulations of a pitching NACA0012 incurring in deep dynamic stall

G Baldan, A Guardone - arxiv preprint arxiv:2405.12036, 2024 - arxiv.org
This study investigates the flow evolution past a pitching NACA0012 airfoil undergoing deep
dynamic stall using a wall-resolved large eddy simulation approach. Numerical results are …

Practical aspects of designing background-oriented schlieren (BOS) experiments for vortex measurements

C Schwarz, JN Braukmann - Experiments in Fluids, 2023 - Springer
Setup-related aspects of background-oriented schlieren (BOS) experiments are discussed
focusing on a sensitivity parameter S, which represents the relation between light deflection …

The effects of turbulence modeling on dynamic stall

G Baldan, F Manara, G Frassoldati, A Guardone - Acta Mechanica, 2025 - Springer
A numerical investigation of the flow evolution over a pitching NACA 0012 airfoil incurring in
deep dynamic stall phenomena is presented. The experimental data at Reynolds number …