Buckling of an imperfect spherical shell subjected to external pressure

被引:16
|
作者
Ismail, M. S. [1 ]
Mahmud, J. [2 ]
Jailani, A. [3 ]
机构
[1] Politekn Sultan Salahuddin Abdul Aziz Shah, Jabatan Kejuruteraan Mekanikal, Shah Alam 40150, Selangor, Malaysia
[2] Univ Teknol MARA, Coll Engn, Sch Mech Engn, Shah Alam 40450, Selangor, Malaysia
[3] Politekn Port Dickson, Jabatan Kejuruteraan Mekanikal, Km 14 Jalan Pantai Si Rusa, Port Dickson 71050, Negeri Sembila, Malaysia
关键词
Spherical shell; Eigenmode imperfection; Single load indentation (SLI) imperfection; Closed-form lower-bound empirical formula; Buckling; Design codes; Knockdown factor; CYLINDRICAL-SHELLS; AXIAL-COMPRESSION; STEEL; LOAD; STABILITY; BEHAVIOR; DESIGN;
D O I
10.1016/j.oceaneng.2023.114118
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
This paper presents numerical results focusing on the buckling behaviour of externally pressurised imperfect spherical shells. The numerical model followed the recommendations of the European Standard EN1993-1-6. A good agreement between the model FE and the experimental results with an average difference of less than 7% was found. The perfect steel spherical shell is then subjected to several imperfection approaches, such as (a) eigenmode imperfection and (b) single load indentation (SLI) imperfection. The eigenmode shape imperfection proves to be the worst imperfection for the externally pressurised spherical shells, yet the SLI is an attractive technique to simulate the realistic imperfection (i.e., dent/dimple). Based on the recommendation of the Eu-ropean Standard EN1993-1-6 for imperfection tolerance, the SLI imperfection was used for the realistic-case imperfection approach for different spherical shell configurations. A lower-bound closed-form empirical for-mula for a spherical shell under external pressure was proposed for the spherical shell with the single load indentation (SLI). The results show that for a shell shape parameter lambda >= 10, the EBC provides a much higher knockdown factor compared to the guidelines of NASA SP-8032, Wagner, and lower-bound closed-form empirical formula (the differences are in the range of 48%-56%).
引用
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页数:12
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