A Basic Study of CFRP Laminates with Embedded Prestrained SMA Foils for Aircraft Structures

Journal of Intelligent Material Systems and Structures

Volumn 16, Issue 2, 2005, Pages 175-185

  Ogisu, Toshimichi ^a   Shimanuki, Masakazu ^a   Kiyoshima, Satoshi ^a   Takeda, Nobuo ^b  

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

Author keywords

CFRP(carbon fiber reinforced plastic); damage behavior; damage suppression effects; delamination; load unload test; recovery stress of SMA; SMA (shape memory alloy); smart material and structural system; transverse crack

Indexed keywords

EID: 84992905428     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1177/1045389X05048908     Document Type: Article

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