Investigation of Stall Flutter Based on Peters-ONERA Aerodynamic Model

The Peters model is used to simulate the linear aerodynamic force and ONERA stall model is used to simulate the nonlinear aerodynamic force. The state-space equation of the aeroelastic system is established by coupling the structural equation. In order to solve problems, Euler predictor corrector me...

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Formato:	Artigo
Idioma:	Chinês
Publicado em:	EDP Sciences 2018-10-01
coleção:	Xibei Gongye Daxue Xuebao
Assuntos:	stall flutter dynamic stall under relaxation iteration bifurcation disturbance aeroelasticity angle of attack
Acesso em linha:	https://www.jnwpu.org/articles/jnwpu/pdf/2018/05/jnwpu2018365p875.pdf
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