PASS/NOZZLE-FEM 3.5. Program Manual |
Fig. 4.6. Coordinates system associated with main shell orientation (global). |
Stiffness at the nozzle end:
Linear, kN/mm | Angular, kN m/° | ||||
KLx | KLy | KLz | KRx | KRy | KRz |
96.2643 | 261.6238 | 211.1924 | 619.0299 | 4688.6240 | 161.6278 |
Flexibility at the nozzle end:
Linear, kN/mm | Angular, kN m/° | ||||
FLx | FLy | FLz | FRx | FRy | FRz |
0.0104 | 0.0038 | 0.0047 | 0.0016 | 2.1328·10-4 | 0.0062 |
Flexibility factors at the nozzle end:
Description | Values | |
Axial from Fy | ka | 2.7824 |
Inplane from Mx | ki | 2.6420 |
Outplane from Mz | ko | 5.0419 |
Torsion from My | kt | 3.1825 |
PASS/NOZZLE-FEM 3.5. Program Manual
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