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                                                Posted:
                            
                                8 years ago                            
                            
                                Jun 15, 2017, 11:16 a.m. EDT                            
                        
                        
                                                    Some problems are still too big to solve. 
Things to try include: getting clever about meshing; invoking symmetries; finding a smaller problem that is close enough to the original. 
Maybe if you explain more what question you are trying to answer people can make more specific suggestions. After all, the objective of simulation is not "simulate X" but rather "find attenuation," "find resonant frequency," "find forces," "optimize dimension," or whatever.
D. W. Greve
DWGreve Consulting                                                
                                                
                            Some problems are still too big to solve. 
Things to try include: getting clever about meshing; invoking symmetries; finding a smaller problem that is close enough to the original. 
Maybe if you explain more what question you are trying to answer people can make more specific suggestions. After all, the objective of simulation is not "simulate X" but rather "find attenuation," "find resonant frequency," "find forces," "optimize dimension," or whatever.
D. W. Greve
DWGreve Consulting                        
                                                
                                                                                                            
                                             
                                            
                            
                                                                                        
                                Mads Herring Jensen
                                                                                                                                                    COMSOL Employee
                                                         
                            
                                                                                                                                                
                         
                                                
    
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                                                Posted:
                            
                                8 years ago                            
                            
                                Jun 21, 2017, 3:21 a.m. EDT                            
                        
                        
                                                    Dear Nguyen
In version 5.3 we have made improvements on several fronts to model large acoustic problems. First of all, there are now predefined iterative solvers that you can enable if your problem is too large. Here you can save a lot of memory.
If you can work in the time domain I suggest you have a look at the convected wave equation interface, if you keep the background flow to be 0, then you basically solve pressure acoustics. The interface uses the DG method and is very memory efficient, it can solve for many million degrees of freedom. Moreover you only need to mesh with lambda/1.5 to lambda/2 so it will help on the mesh side also.
As also suggested make sure to use symmetries, take care of your mes etc.
Best regards
Mads                                                
                                                
                            Dear Nguyen
In version 5.3 we have made improvements on several fronts to model large acoustic problems. First of all, there are now predefined iterative solvers that you can enable if your problem is too large. Here you can save a lot of memory.
If you can work in the time domain I suggest you have a look at the convected wave equation interface, if you keep the background flow to be 0, then you basically solve pressure acoustics. The interface uses the DG method and is very memory efficient, it can solve for many million degrees of freedom. Moreover you only need to mesh with lambda/1.5 to lambda/2 so it will help on the mesh side also.
As also suggested make sure to use symmetries, take care of your mes etc.
Best regards
Mads                        
                                                
                                                                                                            
                                             
                        
                        
                                                
    
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                                                Posted:
                            
                                8 years ago                            
                            
                                Jun 25, 2017, 11:06 p.m. EDT                            
                        
                        
                                                    Thank for your help.
I am trying another solution, could be named as "subsectional computation". I divide the whole domain (560m) into 56 sections (10m length each). The acoustic source is located at the first section, and I can obtain the pressure at the boundary surface between 1st and 2nd section. That data set of pressure is used as initial data of 2nd section and find the pressure at the boundary surface between 2nd and 3rd section, and keep going on until the end.
However, the frequency response of combined section is differed from frequency response of union section. I am trying to figure out why. 
Is there any similar model using this computation method?
Thank you.                                                
                                                
                            Thank for your help.
I am trying another solution, could be named as "subsectional computation". I divide the whole domain (560m) into 56 sections (10m length each). The acoustic source is located at the first section, and I can obtain the pressure at the boundary surface between 1st and 2nd section. That data set of pressure is used as initial data of 2nd section and find the pressure at the boundary surface between 2nd and 3rd section, and keep going on until the end.
However, the frequency response of combined section is differed from frequency response of union section. I am trying to figure out why. 
Is there any similar model using this computation method?
Thank you.