Investigation of Stall Flutter Based on Peters-ONERA Aerodynamic Model

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...

Full description

Bibliographic Details
Format: Article
Language:zho
Published: EDP Sciences 2018-10-01
Series:Xibei Gongye Daxue Xuebao
Subjects:
stall flutter
dynamic stall
under relaxation iteration
bifurcation
disturbance
aeroelasticity
angle of attack
Online Access:https://www.jnwpu.org/articles/jnwpu/pdf/2018/05/jnwpu2018365p875.pdf

Internet

https://www.jnwpu.org/articles/jnwpu/pdf/2018/05/jnwpu2018365p875.pdf

Similar Items