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$$$$ BALOURD  NOTICE  CHAT      11/09/12    21:15:11     7124           
                                             DATE     11/09/12
 
     Procedure BALOURD                      Voir aussi GYRO, CAMPBELL
     ------------------                                     
 
                    BALOURD TAB1 PROMEG   

Objet:
------ 
  

 
         BALOURD computes the response of a rotating machine 
         under unbalanced load
         The calculation can be performed using an eigenmode base.             

   INPUT
 
 TAB1     Table containing:
 
    TAB1.'BASE_MODALE': Table with the real eigenmode base
                        (table generated by VIBR with the option TBAS)
                        If no eigenbase is given, the calculation is
                        directly performed with the matrix
 
    The mass, stiffness, damping and gyroscopic coupling matrices
     can be given either reduced on an eigenmode base or not:  
   
    TAB1.'MASS_PROJ': Mass matrix projected on the eigenmodes base 
    TAB1.'MASSE': Complete mass matrix 
 
    TAB1.'RIGI_PROJ': Stiffness matrix projected on the eigenmodes base 
    TAB1.'RIGIDITE': Stiffness matrix

    TAB1.'AMOR_PROJ':  Damping matrix projected on the eigenmodes base 
    TAB1.'AMORTISSEMENT': Damping matrix

    TAB1.'KROT_PROJ': Antisymetric stiffness due to the rotating damping
                     projected on the eigenmodes base 
    TAB1.'KROTATIF': ntisymetric stiffness due to the rotating damping
 
    TAB1.'GYRO_PROJ': Gyroscopic coupling matrix projected on 
                        the eigenmodes base 
    TAB1.'GYROSCOPIQUE': Gyroscopic coupling matrix

       The gyroscopic coupling matrix must be given for a rotating speed 
       equal to 1 rad/s
     
    The unbalance load can be defined in 2 ways:
 
   1- Only the real part of the unbalance load and the procedure 
      compute the imaginary part assuming the rotating axe is the Ox axes
      (by default)
 
    TAB1.'FBALOURD': Unbalance load for a unitary rotation speed equal
                     to 1 rad/s

    TAB1.'VROTATION': CHPO defined on the same point than the unbalance load
                      which gives the direction of the rotating axe
                     (CHPO component: RX RY RZ)

   2- The user may give boith the real and the imaginary parts of 
       the unbalance load (reduced or not on the eigenmode base)
 
    TAB1.'FBAR_PROJ': Real part of the unbalance load 
                      projected on the eigenmodes base 
    TAB1.'FBAI_PROJ': Imaginary part of the unbalance load 
                      projected on the eigenmodes base 
 
    TAB1.'FBALREEL': Real part of the unbalance load 
    TAB1.'FBALIMAG': Imaginary part of the unbalance load 
    The unbalanbce load must be given for a rotating speed equal to 1 rad/s
                
 
    TAB1.'REPONSE' : Table containing the points for which are saved the results
     (TAB1.'REPONSE').i.'POINT': 
 
    TAB1.'SAUVDEFO': VRAI if the the complete deformed shaped is saved
 
 
    TAB1.'AFFICHAGE': VRAI if the values of the current computed frequency 
          step are plotted during the calculation 

  PROMEG:  LISTREEL containing the rotating speed (unit rad/s) for which are 
              calculated the response of the rotating machine to
              the unbalance load
 
   OUTPUT
 
    TAB1.'REPONSE' : Table containing i indices
     (TAB1.'REPONSE'). i . 'POINT': Points where are calculated the response 
     
         (TAB1.'REPONSE'). i . 'UXREEL': Real part of the UX displacement 
         (TAB1.'REPONSE'). i . 'UYREEL': Real part of the UY displacement 
         (TAB1.'REPONSE'). i . 'UZREEL': Real part of the UZ displacement 
         (TAB1.'REPONSE'). i . 'RXREEL': Real part of the RX rotation 
         (TAB1.'REPONSE'). i . 'RYREEL': Real part of the RY rotation 
         (TAB1.'REPONSE'). i . 'RZREEL': Real part of the RZ rotation 
         (TAB1.'REPONSE'). i . 'UXIMAG': Imaginary part of UX
         (TAB1.'REPONSE'). i . 'UYIMAG': Imaginary part of UY
         (TAB1.'REPONSE'). i . 'UZIMAG': Imaginary part of UZ 
         (TAB1.'REPONSE'). i . 'RXIMAG': Imaginary part of UX
         (TAB1.'REPONSE'). i . 'RYIMAG': Imaginary part of UY
         (TAB1.'REPONSE'). i . 'RZIMAG': Imaginary part of UZ
 
     
         (TAB1.'REPONSE'). i . 'UX': Maximum displacement UX 
         (TAB1.'REPONSE'). i . 'UY': Maximum displacement UY 
         (TAB1.'REPONSE'). i . 'UZ': Maximum displacement UZ 
         (TAB1.'REPONSE'). i . 'RX': Maximum rotation    RX  
         (TAB1.'REPONSE'). i . 'RY': Maximum rotation    RY  
         (TAB1.'REPONSE'). i . 'RZ': Maximum rotation    RZ  
         (TAB1.'REPONSE'). i . 'GAXE': Maximum displacement perpendicular 
         to the rotating axe which correspond to the major axe of the ellipse
         described by the point                              
         (TAB1.'REPONSE'). i . 'PAXE':  Minimum displacement perpendicular 
         to the rotating axe which correspond to the minor axe of the ellipse
         described by the point           
 
      Real and imaginary deformed shaped for each computed rotating speed
      TAB1.'SAUVDEFO': Table containing the deformed shape
      (TAB1.'SAUVDEFO'). i.'FREQROTA' : Rotating speed
      (TAB1.'SAUVDEFO'). i. 'DEFORMEE_REELLE' : Real deformed shape
      (TAB1.'SAUVDEFO'). i. 'DEFORMEE_IMAGINAIRE' : IMaginary deformed shape
  
 

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