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Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load.

机译：加固荷载作用下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 curcular cylindrical shell to carry safely a specified destabilizing load (uniform axial compression, uniform pressure, and torsion) individually applied.

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作者
simitses,george j. aswani, mohan;
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年度 1975
页码 1-104
总页数 104
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Fuselages; Stiffened cylinders; Shells(Structural forms); Dynamic loads; Load distribution; Instability; Thin walls; Compression; Hydrostatic pressure; Torsion; Skin(Structural); Lightweight; Stresses; Yield strength; Ring stiffened cylinders; Trade off analyses; Optimization; Partial differential equations; Matrices(Mathematics); Design;

机译：保险丝;加强圆柱;壳体（结构形式）;动态载荷;载荷分布;不稳定性;薄壁;压缩;静水压力;扭转;表皮（结构）;轻量;应力;屈服强度;环形加强圆柱;折衷分析;优化偏微分方程;矩阵（数学）;设计;

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机译：承受外部静水压力的各向同性单壳和环加筋圆柱壳的优化设计
8. MINIMUM WEIGHT DESIGN OF FUSELAGE TYPE STIFFENED CIRCULAR CYLINDRICAL SHELLS SUBJECT TO UNIFORM AXIAL COMPRESSION [R] . GEORGE J SIMITSES, VARIDDHI UNGBHAKORN 1974

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

Minimum Weight Design of Stiffened Circular Cylindrical Shells Subject to Destabilizing Load.

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