On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds-Reference-Cited by-同舟云学术

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On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds

Published:2017-10 Issue: Volume:74 Page:19-34
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

dos Santos Carlos R.,Pereira Daniel A.,Marques Flávio D.

Funder

São Paulo Research Foundation (FAPESP)

National Council for Scientific and Technological Development (CNPq)

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference22 articles.

1. Unsteady aeroelastic behaviors of rigid airfoils with preset angles of attack;Bichiou;J. Vib. Control,2014

2. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow;Camilo;Aerosp. Sci. Technol.,2013

3. Progress in analysis and prediction of dynamic stall;Carr;J. Aircr.,1988

4. Nonlinear Aeroelastic Behaviour of Aerofoils Under Dynamic Stall;Chantharasenawong,2007

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

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