An experimental investigation on the flow control of the partially stepped NACA0012 airfoil at low Reynolds numbers-Reference-Cited by-同舟云学术

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

Published:2024-08 Issue: Volume:306 Page:118068
ISSN:0029-8018
Container-title:Ocean Engineering
language:en
Short-container-title:Ocean Engineering

Author:

Seyhan Mehmet^ORCID,Akbıyık Hürrem^ORCID

Publisher

Elsevier BV

Reference50 articles.

1. Optimization of horizontal axis wind turbine performance with the dimpled blades by using CNN and MLP models;Abbaskhah;Ocean Eng.,2023

2. Aerodynamics of a flying wing UAV with backward facing stepped wing profile;Abdullah,2017

3. Enhancing vertical axis wind turbine efficiency through leading edge tubercles: a multifaceted analysis;Ahmad;Ocean Eng.,2023

4. Drag and lift reduction of a 3D bluff-body using active vortex generators;Aider;Exp. Fluid,2010

5. Comparison of the linear and spanwise-segmented DBD plasma actuators on flow control around a NACA0015 airfoil;Akbiyik;IEEE Trans. Plasma Sci.,2017

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