Thermomechanically coupled FEM analysis for drape forming process of fighter plane canopy

Hangkong Cailiao Xuebao/Journal of Aeronautical Materials

Volumn 24, Issue 4, 2004, Pages 54-56

  Yan, Yue ^a   Hu, Ping ^b   Liu, Hai Peng ^b  

^a BEIJING INSTITUTE OF AERONAUTICAL MATERIALS   (China)

^b JILIN UNIVERSITY   (China)

Author keywords

Drape forming; Mechanical model of large strain thermomechanically coupling; PC polymer sheet; Static explicit finite element method

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COMPUTER SIMULATION; DEFORMATION; FINITE ELEMENT METHOD; FRICTION; POLYCARBONATES; STRAIN;

BOUNDARY FRICTION; DRAPE FORMING; LARGE STRAIN DEFORMATION; THERMAL MECHANICAL COUPLING;

FIGHTER AIRCRAFT;

EID: 7944227546     PISSN: 10055053     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)