Design, fabrication and testing of a composite bracket for aerospace applications

Composite Structures

Volumn 38, Issue 1-4, 1997, Pages 91-98

  Thuis, H G S J ^a   Biemans, C ^a  

^a NATIONAL AEROSPACE LABORATORY NLR   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE APPLICATIONS; COMPOSITE STRUCTURES; FINITE ELEMENT METHOD; OPTIMIZATION; STRUCTURAL DESIGN; TRANSFER MOLDING;

COMPOSITE BRACKETS;

FLEXIBLE STRUCTURES;

EID: 0031131233     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(97)00045-7     Document Type: Article

References (3)

1. Merazzi, S., Modular finite element analysis tools applied to problems in engineering. Ph.D. thesis 1251, Ecole Polythenique Federale de Lausanne (EPFL), Lausanne, 1994.
2. Arendsen, P., The B2000 Optimization Module: B2OPT. NLR Technical Publication TP 94116 L, published as part of the GARTEUR AG13. Structural Optimization Action Group Report, 1993.
3. Thuis, H. G. S. J., Design stress levels and rough design rules for CFRP structures with concentrated load introductions - an experimental study. NLR technical report TR 97045 L, 1997.