#Turbine A input file #Similar to the NREL CER Phase III 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 3.372 # 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 3.0 # blade number CONE 3.42 # cone angle of rotor RHO 0.002378 HUB 0.04 RD 16.67 RPM_FIXED 71.63 CHORD_BASE 0.0905 CHORD_RELATIVE 2 .5 .000 1. .000 TWIST_RELATIVE 18 0.14 44.67 0.17 39.39 0.22 32.29 0.27 26.56 0.32 21.95 0.37 18.19 0.42 15.10 0.47 12.52 0.52 10.35 0.57 8.50 0.62 6.91 0.67 5.52 0.72 4.32 0.77 3.25 0.82 2.30 0.87 1.45 0.92 0.69 0.97 0.00 #CH_TW # Normalized chord distribution and twist angle along span # 0.0625 6.3 # 0.0792 6.3 # 0.0959 6.3 # 0.1064 5.93 # 0.0984 4.45 # 0.0903 2.96 # 0.0823 1.48 # 0.0743 0.00 # 0.0663 -1.48 # 0.0583 -2.96 #NEG_STALL_DATA #CORRIGAN_EXPN 1 DU_MODEL 1.0 1.0 1.0 22.5 #OUTPROP #turba-prop.in #OUTAERODYN #turba-aerodyn.in PROPFileNames 10 duseg1.dat turbine A at station 1 duseg2.dat turbine A at station 2 duseg3.dat turbine A at station 3 duseg4.dat turbine A at station 4 duseg5.dat turbine A at station 5 duseg6.dat turbine A at station 6 duseg7.dat turbine A at station 7 duseg8.dat turbine A at station 8 duseg9.dat turbine A at station 9 duseg10.dat turbine A at station 10 AIRFOIL_MODE 3 5 ../polardata/pd.s809d 0.21 10 0 1.1 4 00 27 ../polardata/pd.s809d 0.21 15 0 1.1 4 00 18 ../polardata/pd.s809d 0.21 10 0 1.1 4 00 15 ../polardata/CYLINDER.TXT 0.24 0.10 3 0.1 4 00 30 ../polardata/CYLINDER.TXT 0.24 0.10 3 0.1 4 00 30 AIRFOIL_FAMILY 5 0.00 4 1.0 0.02 5 0.955 0.26 1 0.40 0.60 2 0.80 0.95 3 0.20 # adjust the blend function and the airfoil number in column 2 so as to # get the t/c distbn as mentioned in the IEA report USE_AIRFOIL_FAMILY 1 TIPON DP 1 72 0 999 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 23 2 1 1D_SWEEP WRITE_FILES 35 75 85 90 80 95 99 32 # Airfoil data at particular jseg's w/ Re taken from previous analysis run StationRe 1 3 #this number must be the same as that for the AirfoilFileNames line 2 6 9 AirfoilFileNames 3 duwfix2.dat turbine A at station 2 duwfix6.dat turbine A at station 6 duwfix9.dat turbine A at station 9 AlfaMinMaxInc 1 -10 50 2 PrintHeaders Itype 3 # # # # Do things to create lsaf airfoil data tables.---------------------------- # List the lsaf airfoil data tables. # This line also sets a flag that tell propid to write out the data to # these file names once the MakeLSAFAirfoilData line is read. # the file names then follow the number of files # Make the lsaf data files, requires a preceeding MakePROPAirfoilData line. # If the AirfoilFileNames is not input, then this line fails. # For not the moment data is hardwired to specific values (dummy numbers). #MakeOutputAirfoilData #--------------------------------------------------------------------------- MakePROPAirfoilData #ECHO_INPUT DUMP_PROP93 1 9 DUMP_PROPID 21 DUMP_LSAF # writes out the lsaf input file *