Optimum design of dome contour for filament-wound composite pressure vessels based on a shape factor

Composite Structures

Volumn 58, Issue 4, 2002, Pages 469-482

  Liang, Cho Chung ^a   Chen, Hung Wen ^b   Wang, Cheng Huan ^c  

^a DA YEH UNIVERSITY   (Taiwan)

^b NATIONAL DEFENSE UNIVERSITY   (Taiwan)

^c Chung Shan Institute of Science and Technology   (China)

Author keywords

Dome contour; Filament wound; Geodesic; Shape factor; The Tsai Wu failure criterion

Indexed keywords

AEROSPACE INDUSTRY; APPROXIMATION THEORY; DOMES; PRESSURE VESSELS;

SHAPE FACTORS;

COMPOSITE MATERIALS;

DESIGN; FIBER REINFORCED COMPOSITE; OPTIMIZATION; VESSEL;

EID: 0036896619     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00136-8     Document Type: Article

References (23)

1. Optimum design for filament-wound rocket-motor cases
2. Optimum design of a reinforced cylindrical pressure vessel
3. A design method for filament wound GRP vessels and pipework
4. Simplified design techniques for laminated cylindrical pressure vessels under stiffness and strength constraints
5. Optimization of laminated cylindrical pressure vessels under strength criterion
6. Composite pressure vessels with higher stiffness
7. Filament windings composite structure fabrication
8. Design considerations for spiralloy glass-reinforced filament-wound structures as rocket inert parts
9. Rocket case performance optimization
10. Structural design considerations for glass pressure vessels
11. Design of dome for polymeric composite pressure vessels
12. Design of dome contour for filament-wound rocket motor cases
13. Optimum design of helically wound composite pressure vessels
14. Carbon pressure vessel performance with changing dome profiles