Effects of Thermo-Mechanical Loads on Aeroelastic Instabilities of Metallic and Composite Panels

作     者：Erasmo Carrera Maria Cinefra Enrico Zappino Lorenzo Succi 

作者机构：Department of Mechanical and Aerospace Engineering Politecnico di TorinoCorso Duca degli Abruzzi 24 10129 Torino Italy School of Aerospace Mechanical and Manufacturing Engineering RMIT University Melbourne Australia 

出 版 物：《Transactions of Nanjing University of Aeronautics and Astronautics》 (南京航空航天大学学报（英文版）)

年 卷 期：2014年第31卷第2期

页      面：118-122页

核心收录：

学科分类：08[工学] 080101[工学-一般力学与力学基础] 0801[工学-力学（可授工学、理学学位）] 

主　　题：Carrera unified formulation(CUF) panel flutter aeroelasticity aero-thermo-elasticity shell elements 

摘      要：Panel flutter phenomena can be strongly affected by thermal loads,and so a refined aeroelastic model is ***-order shell theories are used as structural *** aerodynamic forces are described using the Piston *** temperature is considered uniform over the thickness of the *** aero-thermo-elastic model is derived in the framework of the Carrera unified formulation(CUF),therefore the matrices are expressed in a compact form using the″fundamental nuclei″.Composite and sandwich structures are considered and different boundary conditions are taken into *** effects of the thermal load on the aeroelastic behavior are investigated.