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USER FATAL MESSAGE 9031
Hi, Trying to run a model with the following fatal error USER FATAL MESSAGE 9031 NOGO ENCOUNTERED IN SUBDMAP SEMG -
Strenght Ratio is Zero but I have a Failurer Index
Hi I am running a FEMAP model of a simple laminate loaded in compression and tension. I have PARAM SRCOMPS YES selected. But when I output the strength ratio they are coming out as 0. I had failure indices and strains but for some reason the SR =0 -
Application of Loads on FEM model to compare with CLT hand calcs
I am looking to compare my hand calculations from my classical laminate theory tool to a FEM model. I am using FEMAP and want to apply a Nx load of 100lb.in. How does this convert into the FEMAP load definition. If I use point load the unit would be lbf correct...- martin555
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- Replies: 1
- Forum: Siemens: Femap
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Exportin Strains from femap
Hi I am currently running a FEMAP model and exporting the forces of a shell model and running a CLT hand calculations to get the strains. I want to compare these strains to the strains in FEMAP. Do I compare them to the normal X and Y strains in FEMAP ?- martin555
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- Replies: 1
- Forum: Siemens: Femap
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Import Material Properties into FEMAP
Hi I have a a model that contains materials properties. I want to update all these material properties with material properties from another model. Both models have the same names for the material properties but different properties. Is there a way to do this automatically.- martin555
- Thread
- Replies: 1
- Forum: Siemens: Femap
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Overall Laminate Strain in Femap
Hi I am looking to output the overall strain of a laminate in FEMAP. Looking to either get the max ply strain of the overall strain in FEMAP interface- martin555
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- Replies: 4
- Forum: Siemens: Femap
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Overall Laminate Strain in Femap
Hi I am looking to output the overall strain of a laminate in FEMAP. Looking to either get the max ply strain of the overall strain in FEMAP interface- martin555
- Thread
- Replies: 3
- Forum: Composite engineering
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Cohesive Elements Simcenter CHEXCZ
I have created a model in which in contains two shell elements and a layer of cohesive elements CHEXCZ in between the shell elements. I am looking to know if I need to merge all the nodes between the three layers or how does the cohesive layer work. -
Cohesive Elements Simcenter 3D Multiphysics Environment (with a SOL401/402)
Hi I am looking to create cohesive elements in NX Simcenter 3D. I don't want to look at the cohesive layer between plies in a laminate I want to look at the cohesive/ bonded joint in-between two different surfaces that are attached e.g foam to skin. I am using Simcenter 3D Multiphysics... -
Reaction Forces at RBE2 elements in NX Simcenter
Hi I am looking to export X,Y and Z forces from a RBE2 element in NX Siemens Simcenter. I have used an RBE2 at a joint that transmits X,Y and Z forces. I am more familiar with PATRAN post processing, in which it had the ability to simply plot the MPC forces in the software and also had the... -
Relative Displacement between two points by removing rigid body motions
Hi I am currently analyzing an engine and want to get the relative displacement of the shaft between two bearings. I have plotted the vertical displacement of the nodes on the shaft but I want to get the relative displacement between the engine bearings. So the nodes at the bearings would have... -
EMA IS USED. INSUFFICIENT MEMORY SPECIFIED FOR EMAINC
Hi I am trying to run a large model in NX Nastran Simcenter I am getting the following error EMA IS USED. INSUFFICIENT MEMORY SPECIFIED FOR EMAINC INCREASE THE MEMORY LIMIT BY 84745 MB FOR BETTER PERFORMANCE. I am not sure where I would increase this value by. Does anyone know how...
