Fabrication and testing of composite isogrid stiffened cylinder

Composite Structures

Volumn 45, Issue 1, 1999, Pages 1-6

  Kim, Thomas D ^a  

^a Asian Off Aerosp Research Devmt   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPRESSION TESTING; CYLINDERS (CONTAINERS); FABRICATION; FRACTURE; STABILITY; STRUCTURAL LOADS;

BUCKLING RESISTANCE; COMPOSITE ISOGRID STIFFENED CYLINDER; ISOGRID STRUCTURE; RIB CRIPPLING; SKIN BUCKLING;

COMPOSITE MATERIALS;

EID: 0032629713     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(98)00124-X     Document Type: Article

References (4)

1. Rehfield F. Continuous filament advanced composite isogrid. AFOSR Contract No. F4962077-C-0077, 1979.
2. Kim T, Harvey J, Koury J, Tracy J. Continuous filament wound isogrid structures for space applications. In: ASM Conference Proceedings, 3-7 August, 1993.
3. Kim T. Investigation of composite isogrid stiffened structures. Phillips Laboratory Technical Report 95-1112, October 1995.
4. Reddy A, Valisetty R, Rehfield L. Continuous filament wound concepts for aircraft fuselage structures. J Aircraft 1985;22:249-55.