Design and optimization of laminated conical shells for buckling

Thin-Walled Structures

Volumn 43, Issue 1, 2005, Pages 107-133

  Goldfeld, Yiska ^a,b   Arbocz, Johann ^a   Rothwell, Alan ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

Buckling load; Conical shells; Filament winding process; Laminated composite materials; Optimization; Response surface

Indexed keywords

BINARY CODES; BUCKLING; FILAMENT WINDING; LAMINATED COMPOSITES; OPTIMIZATION; PROBLEM SOLVING; STIFFNESS; STRUCTURAL LOADS;

BUCKLING LOAD; CONICAL SHELLS; FILAMENT-WINDING PROCESS; RESPONSE SURFACE;

SHELLS (STRUCTURES);

EID: 9644302520     PISSN: 02638231     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.tws.2004.07.003     Document Type: Article

References (20)

1. Almroth BO, Brogan FA, Meller E, Zele F, Petersen HT. Collapse analysis for shells of general shape, user's manual for STAGS-A computer code. Technical report AFFDL TR-71-8; 1973.
2. Goldfeld Y, Arbocz J. Buckling of laminated conical shells taking into account the variations of the stiffness coefficients. AIAA J 2004;42(3):642-649.
3. Baruch M, Arbocz J, Zhang GQ. Laminated conical shells - considerations for the variations of stiffness coefficients. Report LR-671, Faculty of Aerospace Engineering, Delft University of Technology, The Netherlands; April 1992.
4. Baruch M, Arbocz J, Zhang GQ. Laminated conical shells - considerations for the variations of the stiffness coefficients. Proceeding of the 35th AIAA/ASME/ASCE/AHS/ASC S.S.D.M conference, Hilton Head, SC; 1994. p. 2505-16.
5. Wang H, Wang TK. Stability of laminated composite circular conical shells under external pressure. Appl Math Mech Engl Ed 1991;12(12):1153-61.
6. Tong L, Wang TK. Simple solutions for buckling of laminated conical shells. Int J Mech Sci 1992;34(2): 93-111.
7. Tong L, Wang TK. Buckling analysis of laminated composite conical shells. Compos Sci Technol 1993; (47):57-63.
8. Li L. The stability of composite material stiffened conical shells under axial compression. Compos Struct 1997;38(1-4):169-77.
9. Tan T. Torsional buckling analysis of thin and thick shells of revolution. Int J Solids Struct 2000;37: 3055-78.
10. Di Sciuva M, Icardi U. On the buckling analysis of imperfect laminated stiffened conical shells. XII congresso nazionale A.I.D.A.A. Como-Villa Olmo, 20-23 lugilo; 1993.
11. Brown RT, Nachlas JA. Structural optimization of laminated conical shells. AIAA J 1985;23(5):781-7.
12. Myers RH, Montgomery DC. Response surface methodology. New York: Wiley; 1995.
13. Jones RM. Mechanics of composite materials. New York: McGraw-Hill; 1975.
14. Whitney JM. Structural analysis of laminated anisotropic plates. Technomic; 1987.
15. Tong L. Buckling of filament-wound laminated conical shells under axial compression. AIAA J 1999;37(6): 778-81.
16. Goldfeld Y, Sheinman I, Baruch M. Imperfection sensitivity of conical shell. AIAA J 2003;4(3):517-24.
17. Walsh GR. Method of optimization. New York: Wiley; 1975. p. 76-9.
18. Haftka RT, Gürdal Z. Elements of structural optimization, 3rd ed. Dordrecht: Kluwer; 1992.
19. Draper NR, Smith H. Applied regression analysis, 3rd ed. New York: Wiley; 1998.
20. Venkataraman S, Haftka RT, Johnson TF. Design of shells structures for buckling using correction response surface approximations. AIAA/USAF/NASA/ISSMO symposium on multidisciplinary analysis and optimization, 7th, St Louis, MO, Sept 2-4, collection of technical papers. Pt. 2 (A98-39701 10-31). Reston, VA: American Institute of Aeronautics and Astronautics; 1998. p. 1131-44.