An Experiential Optimization Design Method for Orthogonal Rib-Stiffened Thin Walled Cylindrical Shells under Axial Loading

Article Preview

Abstract:

Parametric structural FEA (Finite Element Analysis) models of the orthogonal rib-stiffened thin walled cylindrical shells are established using APDL (ANSYS Parametric Design Language). An experiential optimization design method is then developed based on conclusions of series numerical analysis investigating the effects of parameters’ modification upon buckling loads and modes of the structure. The effects of single design parameter modification under both variational and fixed volume (mass) constraints upon the buckling loads and modes indicate that, only one design scheme is able to obtain maximum buckling load when deployment of the strengthening ribs and volume (mass) parameter were settled previously, and minimum mass would be obtained while this maximum buckling load equals to the required design load. Optimization calculations for aluminum alloy material and layered C/E (Carbon/Epoxy) composite material shells with three layering styles are implemented and discussed, and some useful conclusions are obtained. Method and approach developed in this paper provide certain reference value for the optimal design of such structures.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1773-1783

Citation:

Online since:

October 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Wang XinQing. Structure design[M]. Beijing: Space Navigation Press, 1994: 6-7; 52-56 (In Chinese).

Google Scholar

[2] Huang QiZhen. Missile structurematerialstrength[M]. Beijing: Space Navigation Press, 1996: 9-11; 179-190 (In Chinese).

Google Scholar

[3] P. M. Weaver. Design of laminated composite cylindrical shells under axial compression [J]. Composites, Part B: engineering, 2000(31): 669-679.

DOI: 10.1016/s1359-8368(00)00029-9

Google Scholar

[4] J.W. Hutchinson , M.Y. He. Buckling of cylindrical sandwich shells with metal foam cores [J]. International Journal of Solids and Structures, 2000(37): 6777-6794.

DOI: 10.1016/s0020-7683(99)00314-5

Google Scholar

[5] Navin Jaunky and Norman F. Knight, Jr. Optimal design of general stiffened composite circular cylinders for global buckling with strength constraints [C]. AIAA-97-1402, (1997).

DOI: 10.2514/6.1997-1402

Google Scholar

[6] Y. Goldfeld. Buckling and initial post-buckling of generally stiffened conical shells [C]. AIAA-2006-2275, (2006).

DOI: 10.2514/6.2006-2275

Google Scholar

[7] Jan de Vries. Analysis of localized buckling of cylindrical shell using a hierarchical approach [C]. AIAA-2006-2274, (2006).

Google Scholar

[8] Jan de Vries. Localized buckling of imperfect cylindrical shell, a modified FEM approach [C]. AIAA-2007-2226, (2007).

DOI: 10.2514/6.2007-2226

Google Scholar

[9] David Bushnell. Optimization of an axially compressed ring and stringer stiffened cylindrical shell with a general buckling modal imperfection [C]. AIAA-2007-2216, (2007).

DOI: 10.2514/6.2007-2216

Google Scholar

[10] Cui DeGang. Structure stability design manual [M]. Beijing: Aeronautics Industrial Press, 2006: 178-179; 50-52 (In Chinese).

Google Scholar