A New Plate Buckling Design Formula(2nd Report) : On the Plasticity Correction
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概要
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In the previous paper^<l)>, a new buckling design formula for simply supported plate panels subjected to combined in-plane and lateral loads was suggested. The effect of welding residual stress was also included. For the plasticity correction, the well-known Johnson-Ostenfeld formula was used. In the present study, more advanced formula of the plasticity correction is proposed taking account of edge condition effects. The applicability of the proposed formula is demonstrated by comparing with the present and the conventional result.
- 社団法人日本船舶海洋工学会の論文
著者
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Ham Juh
Hyundai Heavy Industries
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Ham Juh
Hyundai Maritime Research Institute Hynudai Heavy Industries Co. Ltd.
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Paik Jeom
Department Of Naval Architecture And Ocean Engineering Research Institute Of Mechanical Technology P
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Ko Jae
Graduate Student, Department of Naval Architecture, Pusan National University
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Ko Jae
Graduate Student Department Of Naval Architecture Pusan National University
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