A feedback control strategy for the airfoil system under non-Gaussian colored noise excitation-Reference-Cited by-同舟云学术

A feedback control strategy for the airfoil system under non-Gaussian colored noise excitation

Published:2014-09 Issue:3 Volume:24 Page:033117
ISSN:1054-1500
Container-title:Chaos: An Interdisciplinary Journal of Nonlinear Science
language:en
Short-container-title:Chaos

Author:

Huang Yong¹,Tao Gang¹

Affiliation:

1. School of Energy and Power Engineering, Nanjing University of Science and Technology, 200 XiaoLingwei Street, Nanjing 210094, People's Republic of China

Funder

China Postdoctoral Science Foundation

Publisher

AIP Publishing

Subject

Applied Mathematics,General Physics and Astronomy,Mathematical Physics,Statistical and Nonlinear Physics

Link

http://aip.scitation.org/doi/pdf/10.1063/1.4891178

Reference17 articles.

1. T. Theodorsen , NASA Report No. 496, 1935.

2. Stochastic flutter of a panel subjected to random in-plane forces. I- Two mode interaction

3. Stochastic non-linear flutter of a panel subjected to random in-plane forces

4. Random binary (coalescence) flutter of a two-dimensional linear airfoil

5. Bifurcation characteristics of a two-dimensional structurally non-linear airfoil in turbulent flow

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