Instability of Functionally Graded Panels with Structural Damping Under Supersomic Flow
In this study, thermal post-buckling behaviors and linear flutter analysis of Functionally Graded(FG) panels with structural damping under a supersonic airflow are investigated. First-order shear deformation theory (FSDT) is applied to model the panel, and the von-Karman strain-displacement relations are adopted to consider the geometric nonlinearity. In addition, the damping is modeled as the Rayleigh damping, and the first-order piston theory is applied for the supersonic aerodynamic load.
Functionally graded materials(FGMs) Thermal post-buckling Stability boundary Structural Damping Supersonic airflows
Sang-Lae Lee Ji-Hwan Kim
School of Mechanical and Aerospace Engineering, Seoul National University, San 56-1, Shinlim-dong, K Institute of Advanced Aerospace Technology ,School of Mechanical and Aerospace Engineering, Seoul Na
国际会议
青岛
英文
1471-1474
2009-10-09(万方平台首次上网日期,不代表论文的发表时间)