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

Check result by looking at lfemiwe090mech.out
Check result by looking at lfemiwe090therm.out
Check result by looking at savgwe090stress.out

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
Interactive Courseware Development Contact Dr. Kriz
Results above were created by:
http://www.jwave.vt.edu/crcd/kriz/examples/example07/index.html
(Revised September 29, 2000)