Optimal Design of Filament Wound Grid-stiffened Composite Cylindrical Structures

被引:9
作者
Buragohain, M. [1 ]
Velmurugan, R. [2 ]
机构
[1] Adv Syst Lab, Hyderabad 500058, Andhra Pradesh, India
[2] Indian Inst Technol, Composites Technol Ctr, Dept Aerosp Engn, Madras 600036, Tamil Nadu, India
关键词
Filament winding; grid-stiffened shell; lattice cylinder; smeared stiffeners model; buckling; LATTICE STRUCTURES; BUCKLING ANALYSIS; PANELS; SHELLS;
D O I
10.14429/dsj.61.482
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
An integral account of design and analysis of grid-stiffened cylindrical structures is presented. For convenience, a two-phase approach is adopted. In the initial phase, with a view to arriving at a few initial possible optimal configurations, parametric analysis through smeared stiffeners approach is utilised. The ribs, in a filament wound grid-stiffened structure, introduce several additional design elements that result in many possible design configurations; in the initial phase, these design options are efficiently reduced to a few numbers. Finite element modelling is used in the final design and analysis. Rib material is distinct from normal unidirectional composites and this aspect is inherently accounted for in the modelling approaches considered here.
引用
收藏
页码:88 / 94
页数:7
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