9. AVARAGE STRESS IN CRITICAL AREA
Solution Name : 15.07_sim1 : Solution 1
Load Case : Subcase - Static Loads 1
Iteration : Static Step 1
Result : Stress - Elemental, Unaveraged
Units : mN/mm^2(kPa)
Coordinate System : Absolute Rectangular
Elem ID X Coord Y Coord Z Coord Von-Mises
17721 12.854E+0 2.405E+0 16.23314 72.168E+3
17724 12.853E+0 1.959E+0 16.23365 68.754E+3
17759 12.906E+0 2.995E+0 16.19497 58.681E+3
19192 1.332E+0 2.207E+0 16.3736 57.167E+3
19216 1.312E+0 1.918E+0 16.3202 77.818E+3
19297 12.485E+0 1.927E+0 16.35486 76.433E+3
Minimum 57.167E+3
Elem ID 19192
Maximum 77.818E+3
Elem ID 19216
Column Sum 411.021E+3
Column Avg 68.504E+3
10. SUMMARY:
1. MAXIMUM ELEMENT STRESS IS 8.2 E+004 Kpa
WHICH IS LESS THAN THE MATERIAL YIELD STRENGTH
2. AVARAGE STRESS IN CRITICAL AREA IS 68 E+004 Kpa SO BY CAMPARING
WITH THE MATERIAL YIELD STRENGTH, SYSTEM WOULD BE SAFE WITH
SAFTY FACTOR 2.
3. WELDING THROAT THICKNESS MUST BE MINIMUM 0.5” OR MORE