* RLS_NO *
r8.7
* PRE_PROCESSING * MAKE_SYSTEM_MATRICES *
       1                  1               
* SOLVE_EQUATION * POST_PROCESSING *
       1                  1
* STATIC * STEP * AC * TRANSIENT * DISPLACEMENT * NON_LINEAR * TEMP_DEPEND *
    0       0     1       0          0           0
* POTENTIAL * NODAL_FORCE_OPTION *
    2
* TREE_GAUGE *
   -1 
* ORDER_OF_SHEPE_FUNCTIONS *
         2
* ICCG_CONV * ACCEL_FACTOR * DIV_FACTOR * DIV_ITERATIONS * SOLVER * THETA * THETA_NETWOEK * THETA_MOTION *
    1.e-8        1.05            100.          100            0      
* NON_LINERAR_CONV * RELAXATION * NO_ITERATIONS * INIT_OPTION * ICCG_CONV_RATIO * CHECK_B
    1.e-3             1.0            20
* POINTS_IN_1D * POINT_IN_TRIANGLE * MAT_POINTS * 
         3               7               0
* INITIAL_STEP * DATA_TYPE * INITIAL_PHASE *
     -1
* FREQUENCY *
   10.
* INITIAL_PHASE * LAST_PHSE * PHASE_INTERVAL 
      -90.           0.         90.             
* INPUT_MESH_FILE *  UNIT  *
        5             0
* POST_DATA_FILE * ELEM_OUT * NODE_OUT *NUMBER_OUTPUT_MATS * AVERAGE * WIDE *
        5               1          1           0
* MESH * CURRENT * MAGNETIC * FORCE_J_B* FORCE_NODAL * DISP * ELEM * HEAT * MAGNETIZATION *
   1        1         1            0          0             0            0
*   MESH   *   A   *   V   *   B   *   B_INTEG *    J_Q  *
     0         0       0       0         0           0
*  Q_AVERAGE * HEAT  *  MAG_FLUX  * CUR_FLUX *
      0         1            0            0
* FORCE_J_B * FORCE_NODAL *
        0         0
* GEOMETRY * DELTA_Z(m) or DETLA_THETA(deg)* NO_LAYERS *
     0         1.0
*COORDINATE * NO_COORDINATES *
COORDINATE         0
* FAR_BOUNDARY_CONDITION 
        0                     0               
* DISTANCE_JUDGE(m) * Distance for judgement (m)
      1.e-4
* NO_BN0_PLANES *
    2
*     CX        *       CY        *      CZ       *      C(m)   *
      1.0               0.0              0.0             0.0
      0.0               1.0              0.0             0.0
* NO_HT0_PLANES *
    1
*     CX        *       CY        *      CZ       *      C(m)   *
      0.0               0.0              1.0             0.0
* NO_A0_LINE *
    0
* CYCLIC     *  SYMMETRICITY *
     0               1             0          11
* NO_MAT_IDS *  EXTEND_TOTAL *  NO_SMAT_IDS 
     2               0            0
* MAT_ID  *  POTENTIAL * B_H_CURVE_ID * SIGMA * MU  * PACKING *
     1            0           0        5.e7      1.0
* MAT_ID  *  POTENTIAL * B_H_CURVE_ID * SIGMA * MU  * PACKING *
      2           1             0         0.0              1.0
*SOURCE *
SOURCE  
*COIL   * SERIES_NO  *  TIME_ID * NO_ELEMENTS * MOTIN_ID * IN_ROTOR *
COIL         1            0          1              
*UNIF  *   BX(T)    *    BY(T)   *   BZ(T)    * A_FORM *
UNIF        0.           0.           1.         0
*END of COIL *
END
*CIRCUIT *
CIRCUIT
* NO_SERIES * NO_POWER_SUPPLIES *  REGION_FACTOR *  IN_IND *  IN_RES * IN_CON *
        1                1                   8.
* SERIES_IDS *
        1
* SERIES_EXTERNAL_INDUCTANCE *
        0.0
* SERIES_EXTERNAL_RESISTANCE *
        0.0
*  CONNECTION_MATRIX *
        1.0 
* PS_ID    *    TYPE  * TIME_ID *   INITIAL_CURRENT *
     1            0         1                0.0   
* END 0f CIRCUIT
END
*END of SOURCE *
END
* NO_DATA *
      1
* TIME_ID * OPTION *
      1     2
*  AMPLITUDE   *  TCYCLE(s)   *   PHASE(deg)  *
     1.   0.1   0.
