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(
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REDUCED-ORDER MODELING FOR AEROELASTIC SYSTEMS VIA NONLINEAR STATE-SPACE IDENTIFICATION 1)
Zhang Jiaming,Yang Zhijun,Huang Rui()
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图 7. $k_{\rm rf} =0.2$时谐波激励下NACA 0012翼型的ROM验证
Fig. 7. The ROM validation of an NACA 0012 airfoil under harmonic excitation with $k_{\rm rf} =0.2$
