Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model-Reference-Cited by-同舟云学术

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Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model

Published:2018-06 Issue: Volume:423 Page:230-245
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Sales T.P.,Marques Flávio D.,Pereira Daniel A.,Rade Domingos A.

Funder

Brazilian Research Agency

São Paulo Research Foundation

National Institute of Science and Technology of Smart Structures in Engineering

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference40 articles.

1. Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems;Sheeta;J. Aircraft.,2002

2. Nonlinear aeroelasticity;Dowell;J. Aircraft.,2003

3. Limit-cycle oscillation studies of a fighter with external stores;Chen,1998

4. Non-linear aeroelastic prediction for aircraft applications;Henshaw;Prog. Aerosp. Sci.,2007

5. Aeroelastic response of a rigid wing supported by nonlinear spring;O'Neill;J. Aircraft.,1998

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