Herencia 2023a - Revision history

Marherna: Marherna moved page Review 944670586520 to Herencia 2023a

2023-12-05T10:06:30Z

Marherna moved page Review 944670586520 to Herencia 2023a

Jeherencia: Jeherencia moved page Draft Herencia 516249341 to Review 944670586520

2023-05-31T06:04:09Z

Jeherencia moved page Draft Herencia 516249341 to Review 944670586520

Jeherencia at 05:46, 31 May 2023

2023-05-31T05:46:36Z

Jeherencia at 05:42, 31 May 2023

2023-05-31T05:42:32Z

Jeherencia: Created page with "

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 |  style="vertical-align: top;"|[11]
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-|  style="vertical-align: top;"|<span id='_Hlk75767355'></span>L. Meirovitch and M. K. Kwak, M. K., Convergence of the classical Rayleigh-Ritz method and the finite element method, AIAA Journal, 28(8), 1509–1516, 1990. [https://doi.org/10.2514/3.25246 https://doi.org/10.2514/3.25246]
+|  style="vertical-align: top;"|L. Meirovitch and M. K. Kwak, M. K., Convergence of the classical Rayleigh-Ritz method and the finite element method, AIAA Journal, 28(8), 1509–1516, 1990. [https://doi.org/10.2514/3.25246 https://doi.org/10.2514/3.25246]
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 |  style="vertical-align: top;"|[12]

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 Table 5. Non-dimensional buckling loads – unsymmetric cross-ply unstiffened circular cylinders with simply supported edges and under external pressure</div>
-Secondly, results for shells stiffened with longitudinal stiffeners or stringers are presented. <span id='cite-_Ref134446657'></span>[[#_Ref134446657|Table 6]]]]]] gives the non-dimensional buckling coefficient <math display="inline">\frac{{2N}_{x}^{cr}{R}^{2}}{D}\,</math> for isotropic circular cylinders with eccentric stringers with simply supported edges and subjected to axial. The shell is made of a metallic material with <math display="inline">\nu =</math><math>0.3</math>. Results are provided using 10x10 terms in the trigonometric series. <span id='cite-_Ref134446657'></span>[[#_Ref134446657|Table 6]] shows the present method provides identical results to those reported in [1] and in [20] (as cited in [1]).
+Secondly, results for shells stiffened with longitudinal stiffeners or stringers are presented. <span id='cite-_Ref134446657'></span>[[#_Ref134446657|Table 6]] gives the non-dimensional buckling coefficient <math display="inline">\frac{{2N}_{x}^{cr}{R}^{2}}{D}\,</math> for isotropic circular cylinders with eccentric stringers with simply supported edges and subjected to axial. The shell is made of a metallic material with <math display="inline">\nu =</math><math>0.3</math>. Results are provided using 10x10 terms in the trigonometric series. <span id='cite-_Ref134446657'></span>[[#_Ref134446657|Table 6]] shows the present method provides identical results to those reported in [1] and in [20] (as cited in [1]).
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 <div id="_Ref134360064" class="center" style="width: auto; margin-left: auto; margin-right: auto;">
-Table 7. Non-dimensional buckling pressure – isotropic circular cylinders shell with rings, simply supported edges and under external pressure</div>
+Table 7. Non-dimensional buckling pressure – isotropic circular cylinders with rings, simply supported edges and under external pressure</div>
 ==6. Concluding remarks==

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