* RLS_NO *
r10.0
* PRE_PROCESSING * MAKE_SYSTEM_MATRICES *
       1                  1               
* SOLVE_EQUATION * POST_PROCESSING *
       1                  1
* STATIC * STEP * AC * TRANSIENT * DISPLACEMENT * NON_LINEAR * TEMP_DEPEND * STEADY_CURRENT *
        0             0      0               1          0           0
* POTENTIAL * NODAL_FORCE_OPTION * PHI_OPTION * FIXED_COODINATE *
       4
* TREE_GAUGE * REGULARIZATION * RENUMBERING * SCALING * LINE_SERACH * MATRIX_ASYMMETRICITY *
   -1                   0             0         0
* NODE_ORDER * EDGE_ORDER *  METRIC_MOD * QUAD_TRI * CALC_IND *  THIN_ELEM
         1
* ICCG_CONV * ACCEL_FACTOR * DIV_FACTOR * DIV_ITERATIONS * SOLVER * THETA * THETA_NETWOEK * THETA_MOTION *
    1.e-8                 0.            10.          10              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
* NO_STEPS * INITIAL_TIME(s) *  DELTA_TIME(s) * NO_DATA * CYCLIC *
     1        0.0             0.01 
* INITIAL_STEP * LAST_STEP * STEP_INTERVAL * TIME_DIFF * RESTART_FILE_OPTION * CONT *
       1                    1                     1                2
* INPUT_MESH_FILE *  UNIT  * NO_MESH *  MESHLESS *
        0             0
* POST_DATA_FILE * ELEM_OUT * NODE_OUT *NUMBER_OUTPUT_MATS * AVERAGE * WIDE * SUF_OPTION *
        5               1          0           0
* MESH * CURRENT * MAGNETIC * FORCE_J_B * FORCE_NODAL * DISP * ELEM * HEAT * MAGNETIZATION * IRON_LOSS *
   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 * MAGNETIC_ENERGY * IRON_LOSS *
        0         0           
* GEOMETRY * DELTA_Z(m) or DETLA_THETA(deg)* NO_LAYERS *
     0         1.0
*COORDINATE * NO_COORDINATES *
COORDINATE         0
* FAR_BOUNDARY_CONDITION 
        3                     0               
* DISTANCE_JUDGE(m) * Distance for judgement (m)
      1.e-5
* NO_BN0_PLANES *
    0
* NO_HT0_PLANES *
    0
* NO_A0_LINE *
    0
* CYCLIC     *  SYMMETRICITY *
     0               1             0          11
* ELEMENT_TYPE * DIVISION_TYPE * RATIO_TYPE *
     0
* X_AIR_LOWER  * X_MAT_LOWER * X_MAT_UPPER * X_AIR_UPPER *
     -0.1          -0.1           0.1           0.1
* Y_AIR_LOWER  * Y_MAT_LOWER * Y_MAT_UPPER * Y_AIR_UPPER *
     -0.1          -0.1           0.1           0.1
* Z_AIR_LOWER  * Z_MAT_LOWER * Z_MAT_UPPER * YZAIR_UPPER *
     -0.1          -0.1           0.1           0.1
*  XDIV_AIR_LOWER * XDIV_MAT  * XDIV_AIR_UPPER *
         0          20              0
*  YDIV_AIR_LOWER * YDIV_MAT  * YDIV_AIR_UPPER *
         0          20              0
*  ZDIV_AIR_LOWER * ZDIV_MAT  * ZDIV_AIR_UPPER *
         0         20             0
* NO_MAT_IDS *  EXTEND_TOTAL *  NO_SMAT_IDS 
     1               0            0
* MAT_ID  *  POTENTIAL * B_H_CURVE_ID * SIGMA * MU  * PACKING *  ANISOTROPY * IRON_LOSS *
     1                  0                     0                   1.      1.0
*SOURCE *
SOURCE  
*COIL   * SERIES_NO  *  TIME_ID * NO_ELEMENTS * MOTIN_ID * IN_ROTOR *
COIL         1            1          1                                     0   
*UNIF  *   BX(T)    *    BY(T)   *   BZ(T)    * A_FORM *
UNIF        0.           0.           1.         0
*END of COIL *
END
*END of SOURCE *
END
* NO_DATA *
      2
* TIME_ID * OPTION *
      1     0
*   C0    *   C1    *   C2    *   C3     *   C4     *  C5    *   C6    *
    0.      100.0       0.0       0.0        0.0       0.0       0.0
*  TEXP   *   TCYCLE  *
    0.0       0.00
* TIME_ID * OPTION *
      2     0
*   C0    *   C1    *   C2    *   C3     *   C4     *  C5    *   C6    *
    -0.1     2.0       0.0       0.0        0.0       0.0       0.0
*  TEXP   *   TCYCLE  *
    0.0       0.00