Layout optimization of a multi-zoned, multi-layered composite wing under free vibration

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 7286, Issue , 2009, Pages

  Vandervelde, Tyler ^a   Milani, Abbas S ^a  

^a UNIVERSITY OF BRITISH COLUMBIA   (Canada)

Author keywords

Adaptive response surface method; Latin hypercube design; One zone ata time sampling; Structural optimization; Vibration

Indexed keywords

ADAPTIVE RESPONSE SURFACE METHOD; COMPOSITE WING; FIBER MATERIALS; FINITE ELEMENT SIMULATIONS; FREE VIBRATION; FREE VIBRATION BEHAVIOR; FREQUENCY-TUNING; LATIN HYPERCUBE DESIGN; LAYOUT OPTIMIZATION; MULTI-LAYERED; MULTIPLE LAYERS; ONE-ZONE-ATA-TIME SAMPLING; VIBRATION; WOVEN FABRICS;

CONCRETE BRIDGES; FABRICS; SHAPE OPTIMIZATION; SIGNAL PROCESSING; STRUCTURAL OPTIMIZATION; STRUCTURE (COMPOSITION); SURFACE PROPERTIES;

STRUCTURAL DESIGN;

EID: 69649089938     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.813090     Document Type: Conference Paper

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