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5. Nonlinear random response of elastically restrained laminated composite panels at thermo-acoustic en

Nonlinear random response of elastically restrained laminated composite panels at thermo-acoustic en

来源 :The 5th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：csnzz

【摘 要】

：

　　Skin plates are a commonly used form of structural components especially in aerospace applications,which are subjected to thermal loads due to aerodynamic a

【作 者】

：

Yilong Wang Dengqing Cao Jiaqi Peng Huagang Lin 

【机 构】

：

TheSchoolofAstronautics,HarbinInstituteofTechnology,Harbin150001,China

【出 处】

：

The 5th International Conference on Dynamics, Vibration and

【发表日期】

：

2018年7期

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论文部分内容阅读

　　Skin plates are a commonly used form of structural components especially in aerospace applications,which are subjected to thermal loads due to aerodynamic and/or solar radiation heating,and random acoustic loadings due to engine and/or aerodynamic transonic noise.

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