A parametric study on supersonic flutter behavior of laminated composite skew flat panels

Composite Structures

Volumn 69, Issue 1, 2005, Pages 55-63

  Singha, Maloy K ^a   Ganapathi, M ^b,c  

^a Janapara   (India)

^b Paradhur   (India)

^c NONE   (India)

Author keywords

Composite skew plate; Finite element; Flutter; In plane loads; Structural damping; Thermal stress

Indexed keywords

ANGLE MEASUREMENT; BOUNDARY CONDITIONS; DAMPING; EIGENVALUES AND EIGENFUNCTIONS; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; POLYNOMIAL APPROXIMATION; PROBLEM SOLVING; SHEAR DEFORMATION; STRUCTURAL LOADS; STRUCTURAL PANELS; SUPERSONIC FLOW;

FIRST-ORDER HIGH MACH NUMBER APPROXIMATION; STRUCTURAL DAMPING; THERMO-MECHANICAL LOADS;

FLUTTER (AERODYNAMICS);

AEROSPACE TEXTILE; DEFORMATION; FIBER REINFORCED COMPOSITE; FINITE ELEMENT ANALYSIS;

EID: 11244302621     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2004.04.018     Document Type: Article

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