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  5. Nonlinear resonance analysis of FGM truncated conical shell

Nonlinear resonance analysis of FGM truncated conical shell

来源 :The 4th International Conference on Dynamics, Vibration and | 被引量 : 0次 | 上传用户：jieminglin
【摘 要】
：
The nonlinear resonance analysis of a FGM truncated conical shell subjected to the aerodynamic load, in-plane and transverse excitations are investigated in this paper.Material properties are assumed
【作 者】
：
Shaowu Yang Yuxin Hao Wei Zhang 
【机 构】
：
College of Mechanical Engineering, Beijing Information Science and Technology University, Beijing 10
【出 处】
：
The 4th International Conference on Dynamics, Vibration and
【发表日期】
：
2014年8期
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The nonlinear resonance analysis of a FGM truncated conical shell subjected to the aerodynamic load, in-plane and transverse excitations are investigated in this paper.Material properties are assumed to be temperature-dependent and the constituents of FGM truncated conical shell are graded in thickness direction according to a simple power law function in terms of the volume fractions.A first-order piston theory is applied for the hypersonic aerodynamic load.
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