Link to Index Page

Nondimensional buckling loads for compression-loaded stringer-stiffened isotropic cylinders with R/h=500 and simply supported edges

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

This is Fig. 80 in th 2014 NASA report.

Page 122 / 227