Supersonic flutter study of porous 2D curved panels reinforced with graphene platelets using an accurate shear deformable finite element procedure

被引：0
|
作者：
Aditya, S. [1 ]
Haboussi, M. [2 ]
Shubhendu, S. [1 ]
Ganapathi, M. [1 ]
Polit, O. [3 ]
机构：
[1] School of Mechanical Engineering, Vellore Institute of Technology, Vellore,632 014, India
[2] Université Paris 13-CNRS, LSPM, UPR 3407, Villetaneuse,F-93430, France
[3] LEME, UPL, Univ. Paris Nanterre, 50 rue de Sevres, Ville d'Avray,92410, France
来源：
Composite Structures | 2020年 / 241卷
关键词：
Eigenvalues and eigenfunctions - Graphene - Flutter (aerodynamics) - Platelets - Plates (structural components) - Fillers - Fluid structure interaction - Shear flow - Finite element method - Shear deformation;
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