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MINIMUM WEIGHT DESIGN OF FUSELAGE TYPE STIFFENED CIRCULAR CYLINDRICAL SHELLS SUBJECT TO UNIFORM AXIAL COMPRESSION

机译：具有均匀轴向压缩的熔体型加筋圆柱壳的最小重量设计

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摘要

This report contains a technical procedure by which one may design a fuselage-type stiffened thin circular cylindrical shell to carry safely a specified uniform axial compression with minimum weight.

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作者
GEORGE J SIMITSES; VARIDDHI UNGBHAKORN;
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年度 1974
页码 1-149
总页数 149
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Cargo aircraft; Fuselages; Weight reduction; Optimization; Stiffened cylinders; Compressive properties; Structural engineering; Computer programs; Engineering design; Minimum weight design; Cylindrical shells; Computer aided design;

机译：货机;保险丝;减重;优化;加强钢瓶;压缩性能;结构工程;计算机程序;工程设计;最小重量设计;圆柱壳;计算机辅助设计;

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2. Reliability-based optimum design of a welded stringer-stiffened steel cylindrical shell subject to axial compression and bending [J] . Simoes L, Farkas J, Jarmai K Structural and multidisciplinary optimization . 2006,第2期

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3. OPTIMUM DESIGN OF A WELDED STRINGER-STIFFENED STEEL CYLINDRICAL SHELL SUBJECT TO AXIAL COMPRESSION AND BENDING [J] . J. Farkas, K. Jarmai Welding in the World: Journal of the International Institute of Welding: Journal of the International Institute of Welding . 2005,第5a6期

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4. Buckling Analysis and Optimization of Stiffened Cylindrical Shells under Uniform Axial Compression [C] . CHEN Xinghua, LONG Lianchun Fracture and strength of solids VII . 2011

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5. An evaluation of codes and standards related to buckling of cylindrical shells subjected to axial compression, bending and external pressure. [D] . Miller, Clarence Dean. 1994

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6. Robustness of Empirical Vibration Correlation Techniques for Predicting the Instability of Unstiffened Cylindrical Composite Shells in Axial Compression [O] . Eduards Skukis, Gints Jekabsons, Jānis Andersons, 2020

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7. An analytical approach to analyze nonlinear dynamic response of eccentrically stiffened functionally graded circular cylindrical shells subjected to time dependent axial compression and external pressure. Part 1: Governing equations establishment [O] . Dao Van Dung, Vu Hoai Nam 2014

机译：一种分析偏心加固功能梯度圆柱形壳体的非线性动力响应的分析方法，经受依赖性轴向压缩和外压的圆形圆柱形壳体。第1部分：管理方程式建立
8. Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load. [R] . simitses,george j. aswani, mohan 1975

机译：加固荷载作用下加筋圆柱壳的最小重量设计。

MINIMUM WEIGHT DESIGN OF FUSELAGE TYPE STIFFENED CIRCULAR CYLINDRICAL SHELLS SUBJECT TO UNIFORM AXIAL COMPRESSION

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