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Thermal Management of High Powered Solid State Lasers |
Hyper-X and X-43C Hot Structures |
ARES (Mars Scout Proposal) |
Mars EEV |
Jupiter Icy Moons Orbiter (JIMO) |
Mars Reconnaissance Orbiter HiRISE Instrument |
A 7000-node PATRAN model shared with few modifications for both structural and thermal analysis -- many parts imported
from Pro, with geometry re-done to allow auto hex mesh
[from the MIDAS project]:
Pro assembly, PATRAN model, thermal results, structural modal analysis,
stress contours on one part:
A PATRAN model created with a tet mesh direct from a Pro assembly import (about 30 minutes working time from start
of import to having results)
Pro assembly, thermal results, close-up of low temperature part:
[Temperatures in K]
An extremely complex geometry part modelled in both PATRAN and Mechanica from direct import of a single Pro part file:
A model of 14 waveguides each 9 meters long -- Pro import to PATRAN, temperatures from TRASYS/SINDA imported to PATRAN
to get structural deflections
Pro assembly, TRASYS model, thermal results:
Several papers have been published which relate to this process: