Бесплатный постпроцессор

[hr4d 87]

Подскажите, есть ли какой-нить бесплатный постпроцессор, чтобы открыть рез-ты расчетов SW, которые .cwr.

Или еще чем можно открыть?

Изменено 5 декабря 2018 пользователем hr4d

[jtok 814]

Постпроцессора не знаю, но можно сменить расширение на ZIP и открыть в получившемся архиве файл OUT - это текстовый файл вывода результатов расчета. В нем будет что-то типа:

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****************************************************************
****************************************************************
**                                                            **
**                                                            **
**        CCC     OO      SSS    M    M     OO      SSS       **
**       C       O  O    S       MM  MM    O  O    S          **
**       C       O  O     SS     M MM M    O  O     SS        **
**       C       O  O       S    M    M    O  O       S       **
**        CCC     OO     SSS     M    M     OO     SSS        **
**                                                            **
**                                                            **
**                Simulations   V 2 0 1 2                     **
**           Distributed By: SolidWorks Corporation           **
**                3000 Ocean Park Blvd., Suite 2001           **
**               Santa Monica, California 90405               **
**               Telephone Number (310)309-2800               **
**         Copyright 1988-2009 SolidWorks Corporation         **
**                                                            **
****************************************************************
****************************************************************

Problem name: \\Fs\§б§д§а\§і§ґ§¦§¬§­§°§±§­§Ў§і§ґ§Є§¬\_
Date        : 08/01/2012     Time:   14:36:53


SYSTEM OF UNITS:
 International System of Units, SI, is used for all input/output data.
 Common Quantities:
 Length:meter, Mass:kilogram, Time:second, Temperature:kelvin
 Force:newton, Pressure also stress:pascal, Energy:joule, Power:watt

  C O N T R O L  I N F O R M A T I O N                  
   NUMBER OF LOAD CASES  . . . . . . . . . . . (NLCASE)  =           1
   SOLUTION MODE . . . . . . . . . . . . . . . (MODEX)   =           0
      EQ. 0, STATIC ANALYSIS                              
      EQ. 1, BUCKLING ANALYSIS                            
      EQ. 2, DYNAMIC ANALYSIS                             
      EQ. 3, DROP TEST                                    

   SOLVER TYPE . . . . . . . . . . . . . . . . .(ISOL)   =           2
      EQ. 0, DIRECT SPARSE SOLVER                         
      EQ. 1, DIRECT SKYLINE SOLVER                        
      EQ. 2, ITERATIVE SOLVER                             
      EQ. 3, EXPLICIT INTEGRATION                         

   ITERATIVE SOLUTION MODE . . . . . . . . . . (IMODE)   =           2
      EQ. 1, GENERAL                                      
      EQ. 2, MEMORY SAVER (FOR TETRA10)                   
      EQ. 3, ULTRA-MEMORY SAVER (FOR TETRA10)             

   SOLVER CONVERGENCE TOLERANCE  . . . . . . . (CONVR)   =   0.100E-03

   THERMAL LOADING FLAG . . . . . . . . . . . .(ITHERM)  =           0
      EQ. 0, NO THERMAL EFFECTS CONSIDERED                
      EQ. 1, ADD TEMPERATURE EFFECT                       
   GRAVITY LOADING FLAG . . . . . . . . . . . .(IGRAV)   =           0
      EQ. 0, NO GRAVITY LOADING CONSIDERED                
      EQ. 1, ADD GRAVITY LOADING EFFECT                   
   CENTRIFUGAL LOADING FLAG . . . . . . . . . .(ICNTRF)  =           0
      EQ. 0, NO CENTRIFUGAL LOADING CONSIDERED            
      EQ. 1, ADD CENTRIFUGAL LOADING EFFECT               
   IN-PLANE STIFFENING FLAG . . . . . . . . . .(INPLN)   =           0
      EQ. 0, NO IN-PLANE EFFECTS CONSIDERED               
      EQ. 1, IN-PLANE EFFECTS CONSIDERED                  
   SOFT SPRING ADDITION FLAG . . . . . . . . . (ISOFT)   =           0
      EQ. 0, NO SOFT SPRING OPTION                        
      EQ. 1, SOFT SPRING ADDED                            

   SAVE DECOMPOSED STIFFNESS MATRIX FLAG . . . (ISAVK)   =           0
      EQ. 0, DO NOT SAVE DECOMPOSED K                     
      EQ. 1, SAVE DECOMPOSED K                            
   FORM STIFFNESS MATRIX FLAG . . . . . . . . .(IFORMK)  =           0
      EQ. 0, FORM STIFFNESS MATRIX                        
      EQ. 1, USE EXISTING DECOMPOSED STIFFNESS MATRIX     

   SPIN SOFTENING FLAG . . . . . . . . . . . . (ISPIN)   =           0
      EQ. 0, NO SPIN SOFTENING EFFECTS CONSIDERED         
      EQ. 1, SPIN SOFTENING EFFECTS CONSIDERED            
   INERTIA RELIEF FLAG  . . . . . . . . . . . .(IFORMK)  =           0
      EQ. 0, NO INERITA RELIEF EFFECTS CONSIDERED         
      EQ. 1, INERITA RELIEF EFFECTS CONSIDERED            
   RIGID CONNECTIONS FLAG  . . . . . . . . . . (IRIGID)  =           0
      EQ. 0, HINGE CONNECTIONS BETWEEN SOLIDS & SHELLS    
      EQ. 1, RIGID CONNECTIONS BETWEEN SOLIDS & SHELLS    


  T O T A L  S Y S T E M  D A T A                        
   NUMBER OF EQUATIONS . . . . . . . . . . . . . .(NEQ)  =       46611
   NUMBER OF ELEMENTS. . . . . . . . . . . . . . .(NUME) =        7661
   NUMBER OF NODAL POINTS. . . . . . . . . . . . .(NUMNP)=       15546




************************************************************************
*        R E S P O N S E     P R I N T O U T    (LOAD CASE     1)      *
************************************************************************




************************************************************************
*        R E S P O N S E     P R I N T O U T    (LOAD CASE     1)      *
************************************************************************


  STATUS OF THERMAL EFFECTS FOR THIS LOAD CASE:
  ---------------------------------------------

    - Thermal flag is off (no thermal effect)



             D I S P L A C E M E N T S

     NODE X-DISPL.     Y-DISPL.     Z-DISPL.     XX-ROT.      YY-ROT.      ZZ-ROT.


 MINIMUM/MAXIMUM DISPLACEMENTS

  NODE      2176         4967         2126            0            0            0
  MIN.  -3.45824E-03 -2.14595E-03 -7.36511E-04   0.0000       0.0000       0.0000    

  NODE      5456         1133          132            0            0            0
  MAX.   3.06905E-03  3.00938E-04  1.17163E-03   0.0000       0.0000       0.0000    

 MAXIMUM RESULTANT DISPLACEMENT

  NODE      2176
  MAX.   3.69983E-03

 FOR REQUESTED                 (Global Cartesian Coord. System)
    NODES         FX         FY         FZ         MX         MY         MZ
 Total React. 0.8352E+02 0.1023E+05 0.5526E+06 0.0000E+00 0.0000E+00 0.0000E+00
  

 TOTAL STRAIN ENERGY. . . . . . . . . . . =  0.474318E+03


 MAXIMUM NODAL VON MISES STRESS

  NODE      8082
  MAX.     0.43875E+08



   E R R O R    E S T I M A T I O N
   (for requested elements)

   Total Strain Energy (TSE)        =  0.474318E+03
   Total Error Energy (TEE)         =  0.178639E+02
   Ave. Percentage Error (APE)      =  0.135953E+02
     ( APE =  sqrt (TEE/(TSE*2. + TEE)) * 100. )



T O T A L   S O L U T I O N   T I M E (sec) . . . . =      55

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[hr4d 87]

Что-то не вышло так.

Блин Ansys Ensight все походу ест, кроме SW.