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- 藤久保 昌彦
- 広島大学工学部
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- 矢尾 哲也
- 広島大学工学部
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- VARGHESE Balu
- 広島大学大学院
書誌事項
- タイトル別名
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- Buckling/Ultimate Strength of Rectangular Plates Subjected to Combined Inplane Loads
- クミアワセメンナイ カジュウ オ ウケル クケイバン ノ ザクツ サイシュウ
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抄録
Elastoplastic large deflection analyses of a simply supported thick rectangular plate subjected to combined inplane loads such as bi-axial compression and shear have been performed using non-linear finite element method. The ultimate strength interaction curves obtained by FEM analyses are compared with the interaction curves of classification societies to check up to what extent the plastic correction formula is reliable when it is applied to plate panels directly. The following conclusions are drawn from this study: (1) Upper bound of the maximum initial deflection in the actual ship plates can be approximated by w_<0max>=0.1β^2t. (2) For the combined loading cases, loading methods including loading sequences and load control methods have only a negligible effect on the yielding-strength and ultimate-strength interaction curves. (3) Plastic correction method used in the existing classification society rules have applicability to thick plates as an estimation method of ultimate strength on the safe side within the limit of upper bound of actual initial deflection, but in some cases it may give strength on the unsafe side depending on the ratios of applied loads. (4) A simple modification has been proposed as an attempt to shift the estimated buckling strength towards the safe side, and its fundamental effectiveness has been demonstrated.
収録刊行物
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- 西部造船会々報
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西部造船会々報 93 (0), 81-89, 1997
社団法人 日本船舶海洋工学会
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詳細情報 詳細情報について
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- CRID
- 1390282680534895232
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- NII論文ID
- 110007627672
- 20000323242
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- NII書誌ID
- AN00295364
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- ISSN
- 0389911X
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- NDL書誌ID
- 4171595
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可