# Turbine B: Similar to the NREL AWT26 turbine


MODE 1.0            # wind turbine
LTIP 1.0            # tip loss model
LHUB 1.0            # tip loss model
IBR 1.0             # brake state model
ISTL 1.0            # viterna stall model
USEAP  1.0          # swiral suppression
WEXP 0.0000         # no boundary layer
HH  2.00            # tower height
NS_NSEC 10.0  1.0   # number of blade elements/number of sectors
IS1   1.0           # first segment used in analysis
IS2  10.0           # last segment used in analysis
BE_DATA 0.0         # printout blade element data
INCV 0.0            # use TSR
SH 0.0              # shaft tilt effects on crossflow
BN 2.0              # blade number
CONE 4.00           # cone angle of rotor
RHO 0.002057        # Air density (slugs/ft^3)
HUB 0.07            # Normalized hub radius 
RD 43.00            # Blade radius (ft)
RPM_FIXED 57.10     # Rotor revolutions per minute

CH_TW               # Normalized chord distribution and twist angle along span
0.01617       5.848
0.07507       5.393
0.08551       4.825
0.08670       4.008
0.08160       2.879
0.07560       1.762
0.06847       0.819
0.05981       0.254
0.04986       0.076
0.03672       0.027

#CORRIGAN_EXPN 1
DU_MODEL  1  1  1  27.25

PROPFileNames
10
uiucseg1.dat
turbine B at station 1
uiucseg2.dat
turbine B at station 2
uiucseg3.dat
turbine B at station 3
uiucseg4.dat
turbine B at station 4
uiucseg5.dat
turbine B at station 5
uiucseg6.dat
turbine B at station 6
uiucseg7.dat
turbine B at station 7
uiucseg8.dat
turbine B at station 8
uiucseg9.dat
turbine B at station 9
uiucseg10.dat
turbine B at station 10

AIRFOIL_MODE   3
  4
../polardata/airfoil2
  0.26   10   0   1.2   7   0  30
../polardata/airfoil2
  0.26   10   0   1.2   7   0  30
../polardata/airfoil1ext
  0.21   15   0   1.1   7   0  30
../polardata/airfoil3 
  0.18   12   0   1.0   7   0  30
../polardata/airfoil3 
  0.18   12   0   1.0   7   0  30
../polardata/CYLINDER.TXT 
  1.00    0.1   3  0.10  4  00  30

# corrigan insert angle set to 7 cos that is what JLt has done with
# the files that he sent to me

AIRFOIL_FAMILY    6
     0.00  6  1.0
     0.05  1  0.85
     0.30  2  0.40 
     0.75  3  0.20
     0.95  4  0.05
     1.00  5  0.00

#    0.00  4  1.0
#    0.05  1  0.99
#    0.30  1  0.97
#    0.75  2  0.90
#    0.95  3  0.62
#    1.00  3  0.50

USE_AIRFOIL_FAMILY    1

TIPON

DP 1 57 1    999 2

IDES


RPM_DP 1
PITCH_DP 1
WIND_SWEEP 7     50.0    1 2.0
2D_SWEEP
WRITE_FILES 40 45 55 95 100 50

RPM_DP 1
PITCH_DP 1
WIND_SWEEP 7 15 2  1
1D_SWEEP
WRITE_FILES 35 75 85 90 80 95 99 32 36

# Airfoil data at particular jseg's w/ Re taken from previous analysis run
StationRe 1
10  #this number must be the same as that for the AirfoilFileNames line
1
2
3
4
5
6
7
8
9
10

AirfoilFileNames
10         
uiucwfix1.dat
turbine B at station 1
uiucwfix2.dat
turbine B at station 2
uiucwfix3.dat
turbine B at station 3
uiucwfix4.dat
turbine B at station 4
uiucwfix5.dat
turbine B at station 5
uiucwfix6.dat
turbine B at station 6
uiucwfix7.dat
turbine B at station 7
uiucwfix8.dat
turbine B at station 8
uiucwfix9.dat
turbine B at station 9
uiucwfix10.dat
turbine B at station 10

AlfaMinMaxInc  1
-1 20 1
PrintHeaders
Itype 3

MakePROPAirfoilData

#OUTPROP
#turbb-prop.in

#OUTAERODYN
#turbb-aerodyn.in

DUMP_PROP93 1 9
DUMP_PROPID 21
DUMP_LSAF  # writes out the lsaf input file
*