Fabrication and testing of thin composite isogrid stiffened panel

Composite Structures

Volumn 49, Issue 1, 2000, Pages 21-25

  Kim, Thomas D ^a  

^a Asian Office of Aerospace Research and Development   (Japan)

Author keywords

Buckling; Composite isogrid structure; Isogrid stiffened structures

Indexed keywords

BUCKLING; COMPRESSIVE STRENGTH; FAILURE ANALYSIS; STIFFNESS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS; STRUCTURAL PANELS;

BUCKLING RESISTANCE; COMPOSITE ISOGRID STRUCTURES; ISOGRID STIFFENED STRUCTURES;

COMPOSITE STRUCTURES;

EID: 0033896275     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(99)00122-1     Document Type: Article

References (6)

1. Rehfield F. Continuous filament advanced composite isogrid. AFOSR Contract No. F4962077-C-0077, 1979.
2. Reddy A., Valisetty R., Rehfield L. Continuous filament wound concepts for aircraft fuselage structures. J Aircraft. 22:1985;249-255.
3. Kim T, Harvey J, Koury J, Tracy J. Continuous filament wound isogrid structures for space applications. In: 1993 ASM Conference Proceedings. August 1993;3-7.
4. Kim T. Investigation of composite isogrid stiffened structures. Phillips Laboratory Technical Report, October 1995;95:11-12.
5. Kim T. Fabrication and testing of composite isogrid stiffened cylinder. Compos Struct 1999;45.
6. Kim T, Rotz C. Warping of flat composite isogrid panels. In: 1997 IEEE Aerospace Conference Proceedings, February, 1997.