Experiments and numerical analysis of compression after impact (CAI) behavior of CF/PIXA stiffened panels for HSCT structure

Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials

Volumn 14, Issue 3, 2005, Pages 239-261

  Ishikawa, Takashi ^a   Matsushima, Masamichi ^a   Hayashi, Yoichi ^a   Scott, Murray L ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b RMIT UNIVERSITY   (Australia)

Author keywords

Buckling; Delamination resistance; Final failure; Fusion bonding; Heat resistant thermoplastic composites; Nonlinear finite element analysis; Ultrasonic C scan

Indexed keywords

BUCKLING; DELAMINATION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; NONLINEAR SYSTEMS; PLATES (STRUCTURAL COMPONENTS); STRUCTURAL PANELS; THERMOPLASTICS;

DELAMINATION RESISTANCE; FINAL FAILURES; FUSION BONDING; HEAT RESISTANT THERMOPLASTIC COMPOSITES; NONLINEAR FINITE ELEMENT ANALYSIS;

COMPOSITE MATERIALS;

EID: 24944515036     PISSN: 09243046     EISSN: None     Source Type: Journal    
DOI: 10.1163/1568551054922638     Document Type: Article

References (12)

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