Damage suppression system using embedded SMA (Shape Memory Alloy) foils in CFRP laminates

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 5054, Issue , 2003, Pages 192-202

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

^a FUJI HEAVY INDUSTRIES LTD   (Japan)

^b UTSUNOMIYA UNIVERSITY   (Japan)

^c UNIVERSITY OF TOKYO   (Japan)

Author keywords

Aircraft fuselage structure; CFRP(Carbon Fiber Reinforced Plastic); Crack opening displacement; Damage onset strain; Damage suppression behavior; Demonstrator; Recovery stress of SMA; SMA(Shape Memory Alloy); Strain energy release rate; Technical verification

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; EMBEDDED SYSTEMS; FUSELAGES; METAL FOIL; SHAPE MEMORY EFFECT; STRAIN; STRESSES; TENSILE TESTING;

DAMAGE SUPPRESSION SYSTEMS;

LAMINATES;

EID: 0242636305     PISSN: 0277786X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1117/12.483882     Document Type: Conference Paper

References (12)

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