Nonlinear flutter of aerothermally buckled composite shells with damping treatments

Journal of Sound and Vibration

Volumn 324, Issue 3-5, 2009, Pages 556-569

  Shin, Won Ho ^a   Oh, Il Kwon ^b   Lee, In ^c  

^a Samsung Electro Mechanics   (South Korea)

^b Chonnam National University   (South Korea)

^c Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AEROTHERMAL LOADS; AEROTHERMOELASTIC BEHAVIOR; ARC LENGTH METHOD; COMPLEX MODULUS; COMPOSITE PANELS; COMPOSITE SHELL; CONSTRAINED LAYER; CYLINDRICAL COMPOSITE SHELLS; DAMPING LAYERS; DAMPING TREATMENT; DISPLACEMENT FIELD; FINITE ELEMENT ANALYSIS; FLUTTER BOUNDARIES; FREE LAYERS; LAYER-WISE; NONLINEAR FLUTTERS; POST BUCKLING DEFORMATION; POSTBUCKLING BEHAVIOR; VISCOELASTIC DAMPING; VISCOELASTIC LAYERS;

BUCKLING; FLUTTER (AERODYNAMICS); HYPERSONIC AERODYNAMICS; PLATES (STRUCTURAL COMPONENTS); SHELLS (STRUCTURES); THERMAL LOAD;

DAMPING;

EID: 67349094571     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2009.02.022     Document Type: Article

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