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Test15_AD.ipt
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SWRT rotor aerodynamic parameters for FAST certification test #15.
SI SysUnits - System of units for used for input and output [must be SI for FAST] (unquoted string)
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)
DYNIN 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)
NONE HLModel - Hub-loss model (EQUIL only) [PRANdtl or NONE] (unquoted string)
"Wind\SWRT\EOG_01_R.wnd" WindFile - Name of file containing wind data (quoted string)
34.6189 HH - Wind reference (hub) height [TowerHt+Twr2Shft+OverHang*SIN(ShftTilt)] (m)
0.0 TwrShad - Tower-shadow velocity deficit (-)
9999.9 ShadHWid - Tower-shadow half width (m)
9999.9 T_Shad_Refpt - Tower-shadow reference point (m)
1.0 AirDens - Air density (kg/m^3)
1.5100E-05 KinVisc - Kinematic air viscosity (m^2/sec)
1.0000E-03 DTAero - Time interval for aerodynamic calculations (sec)
4 NumFoil - Number of airfoil files (-)
"AeroData\SWRT\TailPlate.dat" FoilNm - Names of the airfoil files [NumFoil lines] (quoted strings)
"AeroData\SWRT\SH3052Mod_AllRe_Hanley.dat"
"AeroData\SWRT\SH3052Mod_AllRe_Elem14_Hanley.dat"
"AeroData\SWRT\SH3052Mod_AllRe_Elem15_Hanley.dat"
15 BldNodes - Number of blade nodes used for analysis (-)
RNodes AeroTwst DRNodes Chord NFoil PrnElm
0.3896 0.00 0.1731 0.213 2 NOPRINT
0.5627 0.00 0.1731 0.213 2 NOPRINT
0.7358 0.00 0.1731 0.213 2 NOPRINT
0.9090 0.00 0.1731 0.213 2 NOPRINT
1.0821 0.00 0.1731 0.213 2 NOPRINT
1.2552 0.00 0.1731 0.213 2 NOPRINT
1.4284 0.00 0.1731 0.213 2 NOPRINT
1.6015 0.00 0.1731 0.213 2 NOPRINT
1.7746 0.00 0.1731 0.213 2 NOPRINT
1.9478 0.00 0.1731 0.213 2 NOPRINT
2.1209 0.00 0.1731 0.213 2 NOPRINT
2.2940 0.00 0.1731 0.213 2 NOPRINT
2.4672 0.00 0.1731 0.213 2 NOPRINT
2.6403 1.60 0.1731 0.201 3 NOPRINT
2.8134 3.20 0.1731 0.181 4 NOPRINT
ReNum