New methodology for evaluating toughness of composite laminates - Investigation of damage resistance

Chinese Journal of Aeronautics

Volumn 16, Issue 2, 2003, Pages 73-79

  Yang, Xu ^a,c   Shen, Zhen ^b   Yan, Ying ^c   Liu, Bing Shan ^c  

^a Shenyang Aircraft Des Res Inst   (China)

^b AIRCRAFT STRENGTH RESEARCH INSTITUTE OF CHINA   (China)

^c BEIHANG UNIVERSITY   (China)

Author keywords

Composite materials; Damage parameter; Damage resistance; Design limit; Impact dent

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; DATA REDUCTION; FRACTURE TOUGHNESS; INDENTATION; LAMINATED COMPOSITES; STRUCTURAL DESIGN;

DAMAGE RESISTANCE;

AIRCRAFT MANUFACTURE;

EID: 0038660057     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(11)60207-0     Document Type: Article

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