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Autodesk CFD Forum;
I have a rather complicated largescale model 1 of 24 section with one curvilinear and 3 flats. Put a 100Pa pressure BC on the "inlet" and a 0 velocity reverse normal on the "outlet". Using variable air material on atmosphere model and set glass as the material on the greenhouse section. Using IV2016 -)> CFD 2016 to analyze. Shouldn't it have created an inside volume and automatically set the inlets and outlets for the velocity fields IAW the BC's ?
I've tried the window material to no avail on the larger curvilinear surface.
Dell Precision T7500 8 core xeons 96GB RAM ... When running the radiation experiment I run out of memory according to CFD at 99% iteration point yet my monitor shows only ~18GB used.
I need to see these flow patterns and not once of dozens of tries has CFD reported back inlets/outlets in the messages and I don't think it is creating the special internal volume. Do I need to run the IV shell command on the greenhouse section?
Any help in this matter will benifit us greatly.
Thanks in advance,
R. Harker
Messages
==============================================
Mesher process started...
Loading model...
Loading mesh sizes and constraints...
Meshing...
Surface meshing... generating surface mesh
Surface meshing... smoothing surface mesh
Volume meshing... creating volume mesh
Volume meshing... optimizing volume mesh
Volume meshing... smoothing volume mesh
Mesh contains 664830 nodes and 3466762 elements.
Performing mesh quality check...
Saving mesh...
Meshing completed.
Updating model database...
Model database updated.
Updating mesh database...
Mesh database updated.
Building solver model file...
Solver file written.
Initializing ...
Control file processing complete
Check Out motion License: Successful
Authorization verified
Processing input ...
Mesh input complete
Processing results input ...
Results input complete
Processing BC input ...
Computing restart BC data ...
Calculating BC data structures ...
Calculate wall distance for 664269 fluid nodes
Wall distance calculation done in (3 + 8) seconds. Max distance = 3.09835e+06
BC data structures complete and saved
Analysis Initialization Complete
Input processing complete
** FINITE ELEMENT SUMMARY FOLLOWS...
664830 Total Nodes, 664269 Fluid Nodes , 561 Solid Nodes
3466762 Total Elements, 3462177 Fluid Elements , 4585 Solid Elements
0 Inlets 0 Outlets 0 Unknowns
*********** ANALYSIS STARTED ***********
Turbulent Compressible Flow is ON
Turbulence model: Standard k-epsilon
Intelligent Wall Formulation: ON
Flat lines detected in Convergence Monitor - Auto Stop.
Begin Post-Processing Calculations ...
Post-Processing Calculations Done
Begin Post-Processing File Output ...
Post-Processing File Output Done
Analysis completed successfully
Solved! Go to Solution.
