A modified Leishman–Beddoes model for airfoil sections undergoing dynamic stall at low Reynolds numbers-Reference-Cited by-同舟云学术

A modified Leishman–Beddoes model for airfoil sections undergoing dynamic stall at low Reynolds numbers

Published:2020-02 Issue: Volume:93 Page:102852
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Boutet Johan,Dimitriadis Grigorios,Amandolese Xavier

Funder

European Union

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference24 articles.

1. Unsteady stalling characteristics of thin airfoils at low Reynolds number;Broeren;Prog. Astronaut. Aeronaut.,2001

2. An insight into the dynamic stall lift characteristics;Choudhry;Exp. Therm Fluid Sci.,2014

3. Dat, R., Tran, C.T., Petot, D., 1979. Modèle phénoménologique de décrochage dynamique sur profil de pale d’hélicoptère. In: 16e Colloque D’aérodynamique Appliquée, Lille, France.

4. Introduction to Nonlinear Aeroelasticity;Dimitriadis,2017

5. Present Capabilities of Predicting Two-Dimensional Dynamic Stall;Ekaterinaris,1995

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