Simplified Design Techniques for Laminated Cylindrical Pressure Vessels under Stiffness and Strength Constraints

Journal of Composite Materials

Volumn 22, Issue 12, 1988, Pages 1156-1169

  Fukunaga, Hisao ^a   Chou, Tsu Wei ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b UNIVERSITY OF DELAWARE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84973220547     PISSN: 00219983     EISSN: 1530793X     Source Type: Journal    
DOI: 10.1177/002199838802201206     Document Type: Article

References (10)

1. Roy, A.K. and S.W. Tsai. “Pressure Vessels, in 'Composites Design,” 3rd ed., S. W. Tsai, ed., Thank Composites, Dayton (1987).
2. Chnstensen, N. and E. Wolcott. “Development and Fabrication of a Graphite/Epoxy Motor Case for Air Launch Missile Applications,” 29th National SAMPE Symposium, pp. 1335-1348 (1984).
3. Fukunaga, H. and M. Uemura. “Optimum Design of Helically Wound Composite Pressure Vessels,” Composite Structures, 1: 31-49 (1983).
4. Verderaime, V. and M. Rhemfurth. “Identification and Management of Filament-Wound Case Stiffness Parameters,” NASA TP 2117 (1983)
5. Verderaime, V. “Development of In Situ Stiffness Properties for Shuttle Booster Filament Wound Case,” NASA TP 2377 (1984).
6. Miki, M. “Material Design of Composite Laminates with Required In-Plane Elastic Properties,” Proc. ICCM IV, pp. 1725-1731 (1982).
7. Fukunaga, H. and Y. Hirano. “Stability Optimization of Laminated Composite Plates under In-Plane Loads,” Proc. ICCM IV, pp. 565-572 (1982)
8. Onoda, J. “Optimal Laminate Configurations of Cylindrical Shells for Axial Buckling,” AIAA J., 23: 1093-1098 (1985)
9. Fukunaga, H. and T.W. Chou “On Laminate Configurations for Simultaneous Failure,” J. Composite Materials, 22 271-286 (1988)
10. Tsai, S.W. and H.T. Hahn Introduction to Composite Materials, Lancaster, PA: Technomic Publishing Co., Inc (1980)