Experimental and numerical analysis of critical buckling load of honeycomb sandwich panels

Journal of Composite Materials

Volumn 44, Issue 24, 2010, Pages 2819-2831

  Kaman, Mete Onur ^a   Solmaz, Murat Yavuz ^a   Turan, Kadir ^b  

^a FIRAT UNIVERSITY   (Turkey)

^b DICLE UNIVERSITY   (Turkey)

Author keywords

buckling analysis; composite material; finite element method.; honeycomb sandwich panel

Indexed keywords

ALUMINUM CORES; BUCKLING ANALYSIS; BUCKLING LOADS; BUCKLING STRENGTH; CELL SIZE; COMPRESSION TESTS; CORE DENSITIES; CORE-CELLS; CRITICAL BUCKLING LOADS; EXPERIMENTAL AND NUMERICAL ANALYSIS; FIBER COMPOSITE; FINITE ELEMENT; FINITE ELEMENT ANALYSIS PROGRAM; HONEYCOMB COMPOSITE; HONEYCOMB CORE; HONEYCOMB PANELS; HONEYCOMB SANDWICH PANELS; IMPREGNATED PAPER; NUMERICAL RESULTS; POLYESTER RESIN; SURFACE PLATES;

ALUMINUM; COMPOSITE MATERIALS; COMPRESSION TESTING; COREMAKING; ELECTROMAGNETIC WAVE ABSORPTION; FINITE ELEMENT METHOD; HONEYCOMB STRUCTURES; POLYESTER RESINS; RESINS; SANDWICH STRUCTURES; STRUCTURAL PANELS;

BUCKLING;

EID: 78650354095     PISSN: 00219983     EISSN: 1530793X     Source Type: Journal    
DOI: 10.1177/0021998310371541     Document Type: Article

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