RESULTS of the [0/90]s Laminate
"Stress Free-Edge" Problem

Check FEM results: lfemiwe090mech.out/ lfemiwe090therm.out
Check stress average results, savgwe090stress.out, plotted below.

NOTE: All stresses are near the laminate free-edge:

  
Stress Sigma-Z Through the Laminate Thickness, Y/B=0.9661.


  
Stress Sigma-HZ Through the Laminate Thickness, Y/B=0.9661.


  
Stress Sigma-Z at the Midplane


Comments / Concerns:

Course content in this section: email Dr. Kriz
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Results above were created by:
http://www.jwave.vt.edu/crcd/kriz/modules/module07/index.html
(Revised September 29, 2000)