Analysis of laminated plates by trigonometric theory, radial basis, and unified formulation

AIAA Journal

Volumn 49, Issue 7, 2011, Pages 1559-1562

  Ferreira, Antonio J M ^a,d   Roque, Carla M C ^a,d   Carrera, Erasmo ^b,e   Cinefra, Maria ^b,e   Polit, Olivier ^c,e  

^a UNIVERSITY OF PORTO   (Portugal)

^b POLITECNICO DI TORINO   (Italy)

^c UNIVERSITÉ PARIS OUEST NANTERRE LA DÉFENSE   (France)

^d Faculty of Engineering   (Portugal)

^e Department of Aeronautic and Space Engineering ^*  (France)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING LOADS; COLLOCATION METHOD; CROSS-PLY LAMINATED PLATES; DEFORMATION THEORY; EDGE CONDITIONS; FREE VIBRATION; GOVERNING EQUATIONS; LAMINATED PLATE; MESHFREE; PRINCIPLE OF VIRTUAL DISPLACEMENTS; RADIAL BASIS; RADIAL BASIS FUNCTIONS; SIMPLY SUPPORTED; STATIC DEFORMATIONS; STRONG FORM; TRIGONOMETRIC THEORY;

BUCKLING; DEFORMATION; EQUATIONS OF MOTION; RADIAL BASIS FUNCTION NETWORKS; VIBRATION ANALYSIS;

LAMINATING;

EID: 79959735595     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050888     Document Type: Article

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