基于非线性状态空间辨识的气动弹性模型降阶 1)
张家铭,杨执钧,黄锐(
)
)
REDUCED-ORDER MODELING FOR AEROELASTIC SYSTEMS VIA NONLINEAR STATE-SPACE IDENTIFICATION 1)
Zhang Jiaming,Yang Zhijun,Huang Rui()
)
图 9. BACT机翼颤振边界对比
Fig. 9. Comparison of the flutter boundaries of the BACT wing
