Application of deflected leading and trailing edges to pitching airfoils and cycloidal rotor-Reference-Cited by-同舟云学术

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Application of deflected leading and trailing edges to pitching airfoils and cycloidal rotor

Published:2024-05 Issue: Volume:308 Page:118393
ISSN:0196-8904
Container-title:Energy Conversion and Management
language:en
Short-container-title:Energy Conversion and Management

Author:

Shi Lei,Wang Yefang,Wang Mengcheng,Zhang Desheng

Funder

China Postdoctoral Science Foundation

Excellent Youth Foundation of Jiangsu Scientific Committee

Jiangsu Province Natural Science Foundation

Senior Talent Foundation of Jiangsu University

Publisher

Elsevier BV

Reference39 articles.

1. A review on fluid dynamics of flapping foils;Wu;Ocean Eng,2020

2. Flow field studies on a micro-air-vehicle-scale cycloidal rotor in forward flight;Lind;Exp Fluids,2014

3. Numerical investigations on unsteady vortical flows and separation-induced transition over a cycloidal rotor at low Reynolds number;Shi;Energ Conver Manage,2022

4. Control of dynamic flow field around a pitching NACA633− 618 airfoil by a DBD plasma actuator;Fukumoto;Int J Heat Fluid Flow,2016

5. Aerodynamic performance improvement of a pitching airfoil via a synthetic jet;Wang;European J Mech-B/Fluids,2020

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Application and evaluation of dynamic Bradshaw coefficient in shear stress transport turbulence model for hydraulic machinery;Physics of Fluids;2024-07-01

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