Assessment of added mass effects on flutter boundaries using the Leishman–Beddoes dynamic stall model-Reference-Cited by-同舟云学术

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Assessment of added mass effects on flutter boundaries using the Leishman–Beddoes dynamic stall model

Published:2010-07 Issue:5 Volume:26 Page:814-840
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Peiró J.,Galvanetto U.,Chantharasenawong C.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference27 articles.

1. A synthesis of unsteady aerodynamic effects including stall hysteresis;Beddoes;Vertica,1976

2. Representation of airfoil behaviour;Beddoes;Vertica,1983

3. Practical computation of unsteady lift;Beddoes;Vertica,1984

4. Non-linear analysis of stall flutter based on the ONERA aerodynamic model;Beedy;Aeronautical Journal,2003

5. Flow-induced Vibration;Blevins,2001

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1. Flutter investigation and deep learning prediction of FG composite wing reinforced with carbon nanotube;Curved and Layered Structures;2024-01-01

2. Active Stall Flutter Suppression for a Revised Leishman–Beddoes Model;Journal of Aerospace Engineering;2024-01

3. A novel dynamic stall model based on Theodorsen theory and its application;Renewable Energy;2022-06

4. Dynamical characterization of fully nonlinear, nonsmooth, stall fluttering airfoil systems;Nonlinear Dynamics;2022-01-08

5. Aeroservoelasticity of an Airfoil with Parametric Uncertainty and Subjected to Atmospheric Gusts;AIAA Journal;2021-11

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