--------- AeroDyn v14.04.* INPUT FILE ------------------------------------------------------------------------- NREL 5.0 MW offshore baseline aerodynamic input properties. "BEDDOES" StallMod - Dynamic stall included [BEDDOES or STEADY] (unquoted string) "NO_CM" UseCm - Use aerodynamic pitching moment model? [USE_CM or NO_CM] (unquoted string) "EQUIL" InfModel - Inflow model [DYNIN or EQUIL] (unquoted string) "SWIRL" IndModel - Induction-factor model [NONE or WAKE or SWIRL] (unquoted string) 0.005 AToler - Induction-factor tolerance (convergence criteria) (-) "PRANDtl" TLModel - Tip-loss model (EQUIL only) [PRANDtl, GTECH, or NONE] (unquoted string) "PRANDtl" HLModel - Hub-loss model (EQUIL only) [PRANdtl or NONE] (unquoted string) "NEWTOWER" TwrShad - INSTEAD OF: 0.0 TwrShad - Tower-shadow velocity deficit (-) True TwrPotent - Calculate tower potential flow (flag) INSTEAD OF 9999.9 ShadHWid - Tower-shadow half width (m) False TwrShadow - Calculate tower shadow (flag) INSTEAD OF 9999.9 T_Shad_Refpt- Tower-shadow reference point (m) "NRELOffshrBsline5MW_Onshore_AeroDyn_Tower.dat" TwrFile - Tower drag file name (quoted string) True CalcTwrAero - Calculate aerodynamic drag of the tower at the ElastoDyn nodes. TwrPotent must be true. 1.225 AirDens - Air density (kg/m^3) 1.464E-05 KinVisc - Kinematic air viscosity [CURRENTLY IGNORED] (m^2/sec) "default" DTAero - Time interval for aerodynamic calculations (sec) 8 NumFoil - Number of airfoil files (-) "AeroData/Cylinder1.dat" FoilNm - Names of the airfoil files [NumFoil lines] (quoted strings) "AeroData/Cylinder2.dat" "AeroData/DU40_A17.dat" "AeroData/DU35_A17.dat" "AeroData/DU30_A17.dat" "AeroData/DU25_A17.dat" "AeroData/DU21_A17.dat" "AeroData/NACA64_A17_trialFLAPnew2.dat" 17 BldNodes - Number of blade nodes used for analysis (-) RNodes AeroTwst DRNodes Chord NFoil PrnElm 2.8667000E+00 1.3308000E+01 2.7333000E+00 3.5420000E+00 1 NOPRINT 5.6000000E+00 1.3308000E+01 2.7333000E+00 3.8540000E+00 1 NOPRINT 8.3333000E+00 1.3308000E+01 2.7333000E+00 4.1670000E+00 2 NOPRINT 1.1750000E+01 1.3308000E+01 4.1000000E+00 4.5570000E+00 3 NOPRINT 1.5850000E+01 1.1480000E+01 4.1000000E+00 4.6520000E+00 4 NOPRINT 1.9950000E+01 1.0162000E+01 4.1000000E+00 4.4580000E+00 4 NOPRINT 2.4050000E+01 9.0110000E+00 4.1000000E+00 4.2490000E+00 5 NOPRINT 2.8150000E+01 7.7950000E+00 4.1000000E+00 4.0070000E+00 6 NOPRINT 3.2250000E+01 6.5440000E+00 4.1000000E+00 3.7480000E+00 6 NOPRINT 3.6350000E+01 5.3610000E+00 4.1000000E+00 3.5020000E+00 7 NOPRINT 4.0450000E+01 4.1880000E+00 4.1000000E+00 3.2560000E+00 7 NOPRINT 4.4550000E+01 3.1250000E+00 4.1000000E+00 3.0100000E+00 8 NOPRINT USER 4.8650000E+01 2.3190000E+00 4.1000000E+00 2.7640000E+00 8 NOPRINT USER 5.2750000E+01 1.5260000E+00 4.1000000E+00 2.5180000E+00 8 NOPRINT USER 5.6166700E+01 8.6300000E-01 2.7333000E+00 2.3130000E+00 8 NOPRINT USER 5.8900000E+01 3.7000000E-01 2.7333000E+00 2.0860000E+00 8 NOPRINT USER 6.1633300E+01 1.0600000E-01 2.7333000E+00 1.4190000E+00 8 NOPRINT USER