Henrik Sönnerlind
                                                                                                                                                    COMSOL Employee
                                                         
                            
                                                                                                                                                
                         
                                                
    
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                                                Posted:
                            
                                6 years ago                            
                            
                                11 févr. 2020, 01:07 UTC−5                            
                        
                        Updated:
                            
                                6 years ago                            
                            
                                11 févr. 2020, 01:20 UTC−5                            
                        
                        
                                                    Hi Theodore,
The reason Continuity is not available for boundary-to-boundary in the Shell interface is that the degree of freedom values should not be equal. Thickness and offset must also be taken into account.
You can solve your problem in two different ways. One is to use contact with adhesion, and having the adhesion being always active. The other one is to connect the degrees of freedom using an extrusion coupling operator mapping from one boundary to another. You then prescribe the displacements and rotations on one side in terms of those on the other. Rotations should be equal, while the displacements will also contain terms from the mid-surface distance and rotation.
The situation you describe is however interesting. We will look into adding a more natural 'Continuity-like' condition for modeling it.
Regards,
Henrik
    -------------------
    Henrik Sönnerlind
COMSOL                                                
 
                                                
                            Hi Theodore,
The reason Continuity is not available for boundary-to-boundary in the Shell interface is that the degree of freedom values should not be equal. Thickness and offset must also be taken into account.
You can solve your problem in two different ways. One is to use contact with adhesion, and having the adhesion being always active. The other one is to connect the degrees of freedom using an extrusion coupling operator mapping from one boundary to another. You then prescribe the displacements and rotations on one side in terms of those on the other. Rotations should be equal, while the displacements will also contain terms from the mid-surface distance and rotation.
The situation you describe is however interesting. We will look into adding a more natural 'Continuity-like' condition for modeling it.
Regards,  
Henrik                        
                                                
                                                                                                            
                                             
                                            
                                                
    
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                                                Posted:
                            
                                6 years ago                            
                            
                                17 févr. 2020, 09:35 UTC−5                            
                        
                        
                                                    Hej Henrik,
Appreciate the reply. I tried the approach described related to adhesion.
Thing is, the model for an eigenfrequency analysis shows mode shapes that are separate. For each eigenfrequency only one domain from the whole assembly has a mode shape. It seems as the eigenfrequencies are calculated for each part separately. I used extra pairs so as to restate previous continuity from each domain union but with or without them the results remain the same. I believe I have checked all parameters so could you provide your opinion about it.
                                                                                        Thank you for your time
                                                 
                                                
                            Hej Henrik,
Appreciate the reply. I tried the approach described related to adhesion.
Thing is, the model for an eigenfrequency analysis shows mode shapes that are separate. For each eigenfrequency only one domain from the whole assembly has a mode shape. It seems as the eigenfrequencies are calculated for each part separately. I used extra pairs so as to restate previous continuity from each domain union but with or without them the results remain the same. I believe I have checked all parameters so could you provide your opinion about it.
                                                                                            Thank you for your time                        
                                                
                        
                                                
                                                                                                            
                                             
                        
                        
                            
                                                                                        
                                Henrik Sönnerlind
                                                                                                                                                    COMSOL Employee
                                                         
                            
                                                                                                                                                
                         
                                                
    
        Please login with a confirmed email address before reporting spam
     
    
 
                                                Posted:
                            
                                6 years ago                            
                            
                                18 févr. 2020, 03:56 UTC−5                            
                        
                        
                                                    Hi Theodore,
When you combine contact with eigenfrequency analysis, you should run an Eigenfrequnecy, Prestressed study in order to get the correct linearization point for the eigenfrequency analysis.
Regards,
Henrik
    -------------------
    Henrik Sönnerlind
COMSOL                                                
 
                                                
                            Hi Theodore,
When you combine contact with eigenfrequency analysis, you should run an *Eigenfrequnecy, Prestressed* study in order to get the correct linearization point for the eigenfrequency analysis.
Regards,  
Henrik