![Nondimensional buckling loads for external-pressure-loaded angleply cyl. with [(+60,-60)6]s, R/h=500, simply-supported edges](../mediafiles/l205.jpg)
|
|
||
|
|
|
|
From:
Michael P. Nemeth (NASA Langley Research Center, Hampton, Virginia, USA), “Buckling analysis for stiffened anisotropic circular cylinders based on Sanders’ nonlinear shell theory”, NASA/TM-2014-218176, March 2014
The upper black curve is from Sanders' equations with dead pressure.
This is Fig. 127 in the 2014 NASA report.
Page 205 / 444