Example 11, Slide 31: STAGS model of the same optimized complexly corrugated cylindrical shell with smoothing under uniform axial compression

Fig. 53 from the 2014 GENOPT paper. Top two frames: The huge STAGS model of the optimized specific case, narw96updown with smoothing. Bottom frame: the critical buckling mode and load factor, 1.499. Compare with the bottom frame in the previous figure. There is good agreement between the predictions of STAGS and HUGEBOSOR4.

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