Investigations on the use of a KFm-4 profile to improve the energy extraction performance of a fully-activated flapping foil

A Boudis, O Guerri, AC Bayeul-Lainé, H Oualli… - Ocean …, 2024 - Elsevier
Numerical simulations are performed to evaluate the effects of KFm-4 profile geometry,
reduced frequency, and Reynolds number on the energy extraction performance of a fully …

An experimental investigation on the flow control of the partially stepped NACA0012 airfoil at low Reynolds numbers

M Seyhan, H Akbıyık - Ocean Engineering, 2024 - Elsevier
An experimental study of flow control around a NACA0012 airfoil modified with fully and
partially step geometry was conducted at Reynolds numbers of 6× 10 4 and 1.2× 10 5 …

Experimental investigation of Multi-Step Airfoils in Low Reynolds Numbers Applications

MA Aziz, OA Gaheen, E Benini, AM Elsayed - Heliyon, 2024 - cell.com
This study provides a detailed analysis of the aerodynamic performance of various airfoil
configurations, focusing on lift coefficient, stall characteristics, and maximum lift-to-drag ratio …

Intelligent aerodynamic modelling method for steady/unsteady flow fields of airfoils driven by flow field images based on modified U-Net neural network

B Mi, W Cheng - Engineering Applications of Computational Fluid …, 2025 - Taylor & Francis
An intelligent modelling method driven by flow field images for predicting steady and
unsteady flow filed around aerofoils has been developed. Signed Distance Field (SDF) …

Study on the application of 3D imaging based on the γ-photon silk thread method for visualisation and detection of flow fields

M Yao, M Wang, M Zhao, R Guo, B Ma - Displays, 2024 - Elsevier
As a flow display technique, the silk thread method can clearly show the state of the flow
field. However, displaying the state of the flow field in industrial closed metal cavities is …

Implementation of a PAFV turbulence model for airfoil flow simulation on OpenFOAM

W Yan, Z Sun, Y Sun, X Tian - Physica Scripta, 2024 - iopscience.iop.org
To further develop a more effective turbulence model and to improve the calculation
accuracy of the flow around airfoil, a new PAFV turbulence model has here been …

Aerodynamics of a flying wing UAV with backward facing stepped wing profile

SM Abdullah, A Abdullah, MA Shehzad… - … on Applied Sciences …, 2017 - ieeexplore.ieee.org
A flying wing possesses no definite fuselage and no horizontal tail surfaces resulting in
lesser drag surfaces, a larger wing area with a better range and endurance as compared to …

[引用][C] Contribution à l'amélioration des performances aérodynamiques des ailes battantes

A Boudis - 2021