* RLS_NO *
r9.2
* 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       0            2               1              0            1
* POTENTIAL * NODAL_FORCE_OPTION * PHI_OPTION *
    2              0                   1
* TREE_GAUGE *
   -1 
* ORDER_OF_SHEPE_FUNCTIONS *
         1
* ICCG_CONV * ACCEL_FACTOR * DIV_FACTOR * DIV_ITERATIONS * SOLVER * THETA *
    1.e-6      -1.1            10.          10             0          1.0
* NON_LINERAR_CONV * RELAXATION * NO_ITERATIONS * INIT_OPTION * ICCG_CONV_RATIO * CHECK_B
    1.e-3             0.8           20              0              1.e-4
* POINTS_IN_1D * POINT_IN_TRIANGLE * MAT_POINTS * 
         3               7               1    
* INITIAL_STEP * DATA_TYPE * INITIAL_PHASE * 
    -1                0              0.
* NO_STEPS * INITIAL_TIME(s) *  DELTA_TIME(s) *
  1          -1.                 1.
* INITIAL_STEP * LAST_STEP * STEP_INTERVAL * TIME_DIFF *
      1            1           1            3
* INPUT_MESH_FILE *  UNIT  *
        5             0
* POST_DATA_FILE * ELEM_OUT * NODE_OUT *NUMBER_OUTPUT_MATS * AVERAGE * WIDE * SUF_OPTION *
        5               1         1          5                 0        0       1
8  9  10  12 16
* MESH * CURRENT * MAGNETIC * FORCE_J_B* FORCE_NODAL * DISP * ELEM * HEAT * MAGNETIZATION *
   1        1         1            0          0         1      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         0            0            0
* FORCE_J_B * FORCE_NODAL *
        0         1
* GEOMETRY * DELTA_Z(m) or DETLA_THETA(deg)* NO_LAYERS *
     4         0.042
*COORDINATE * NO_COORDINATES *
COORDINATE         0
* FAR_BOUNDARY_CONDITION 
        0                                   
* DISTANCE_JUDGE(m) * Distance for judgement (m)
      1.e-5
* NO_BN0_PLANES *
    1
*     CX        *       CY        *      CZ       *      C(m)   *
   0.                    0.               1.              0.
* NO_HT0_PLANES *
    0
* NO_A0_LINE *
    0
* CYCLIC  *  SYMMETRICITY * DIVISION * SURFACE_MAT_ID * FITTNESS * LINE_INPUT *
     2               1          32        -1             0.1         0
*   ANGLE(deg) *
   30.
* NUMBER_SLIDING_FACES *
   2
* DIVISION * SURFACE_MAT_ID * FITNESS *
   32          1               0.1
* DIVISION * SURFACE_MAT_ID * FITNESS *
   32          2               0.1
* NO_REGULAR_MESH *
   1
* VELOCITY * REGULAR_NDIV * REGULAR_NMAT *
     36000.         32            1
* MAT_ID_NOS *
   12
* NO_MAT_IDS *  EXTEND_TOTAL *  NO_SMAT_IDS  *
     9              0              0
* MAT_ID  *  POTENTIAL * B_H_CURVE_ID *  SIGMA  *     MU     * PACKING *
* COIL
     8            0           0         0.0      1.0 
* YOKE
     9            0           1         0.0     1000.0
* YOKE
    10            0           1         0.0     1000.0
* AIR-STATOR
    11            0           0         0.0     1.0
* ROTOR
    12            0           1         0.1e8   1000.0
* AIR-ROTOR
    13            0           0         0.00    1.0
    14            0           0         0.00    1.0
    15            0           0         0.00    1.0
    16            0           1         0.      1000.0         
*SOURCE *
SOURCE  
*SDEFCOIL  *SERIES_NO *NO_PARTS * IN_ROTOR *
SDEFCOIL          1      1           0
* MAT_ID * S_MAT_ID1 * S_MAT_ID2 * S_MAT_ID3 * S_MAT_ID4 * CURRENT *  SIGMA  *
    8          21          22         23            24       20.       5.e7
*CIRCUIT *
CIRCUIT
* NO_SERIES * NO_POWER_SUPPLIES *  REGION_FACTOR *  IN_IND *  IN_RES * IN_CON *
        1                1               24.
* SERIES_IDS *
        1 
* SERIES_EXTERNAL_INDUCTANCE *
       0.0
* SERIES_EXTERNAL_RESISTANCE *
       0.0
*  CONNECTION_MATRIX *
        1.0
* PS_ID    *    TYPE  * TIME_ID *   INITIAL_CURRENT * STATOR_OR_ROTOR * 
     1            0         1                  
* END 0f CIRCUIT
END
*END of SOURCE *
END
* NO_DATA *
      2
* TIME_ID * OPTION *
      1       0
*   C0    *   C1    *   C2    *   C3     *   C4     *  C5    *   C6    *
    10.0       0.0       0.0       0.0        0.0       0.0       0.0
*  TEXP   *   TCYCLE  *
    0.0       0.00
* TIME_ID * OPTION *
      11     0
*   C0    *   C1    *   C2    *   C3     *   C4     *  C5    *   C6    *
    0.0       0.       0.0       0.0        0.0       0.0       0.0
*  TEXP   *   TCYCLE  *
    0.0       0.00
* MOTION *  NO_MOTIONS *
MOTION        1
*  MOTIN_ID  * X_TIME_ID * Y_TIME_ID * Z_TIME_ID * PHI_TIME_ID * COORDINATE *
     1            0         0           0            11               0
* GLOBAL_MOTION_ID * SUBERI_S *
     1
* NO_CURVES *
     1
* BH_CURVE_ID * NO_DATA *
     1             39       
*   H_AT/M     *      B_T    *
0.0     0.0
27.     0.01
58.     0.025
100.    0.05
153.    0.10
185.    0.15
205.    0.20
233.    0.30
255.    0.40
285.    0.50
320.    0.60
355.    0.70
405.    0.80
470.    0.90
555.    1.00
673.    1.10
836.    1.20
1065.   1.30
1220.   1.35
1420.   1.40
1720.   1.45
2130.   1.50
2670.   1.55
3480.   1.60
4500.   1.65
5950.   1.70
7650.   1.75
10100.  1.80
13000.  1.85
15900.  1.90
21100.  1.95
26300.  2.00
32900.  2.05
42700.  2.10
61700.  2.15
84300.  2.20
110000. 2.25
135000. 2.30
6262000.  10.0