diff --git a/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat b/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat index 79485b41d..35d9155ec 100644 --- a/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat +++ b/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat @@ -10,6 +10,7 @@ False Echo - Echo the input to ".AD.ech"? (flag True TwrAero - Calculate tower aerodynamic loads? (flag) False FrozenWake - Assume frozen wake during linearization? (flag) [used only when WakeMod=1 and when linearizing] False CavitCheck - Perform cavitation check? (flag) [AFAeroMod must be 1 when CavitCheck=true] +False Buoyancy - Include buoyancy effects? (flag) False CompAA - Flag to compute AeroAcoustics calculation [only used when WakeMod=1 or 2] "unused" AA_InputFile - Aeroacoustics input file ====== Environmental Conditions =================================================================== @@ -57,22 +58,31 @@ True UseBlCm - Include aerodynamic pitching moment in calcul "NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-) "NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2] "NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3] -====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True] - 12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True] -TwrElev TwrDiam TwrCd TwrTI (used only with TwrShadow=2) -(m) (m) (-) (-) -0.0000000E+00 6.0000000E+00 1.0000000E+00 1.0000000E-01 -8.5261000E+00 5.7870000E+00 1.0000000E+00 1.0000000E-01 -1.7053000E+01 5.5740000E+00 1.0000000E+00 1.0000000E-01 -2.5579000E+01 5.3610000E+00 1.0000000E+00 1.0000000E-01 -3.4105000E+01 5.1480000E+00 1.0000000E+00 1.0000000E-01 -4.2633000E+01 4.9350000E+00 1.0000000E+00 1.0000000E-01 -5.1158000E+01 4.7220000E+00 1.0000000E+00 1.0000000E-01 -5.9685000E+01 4.5090000E+00 1.0000000E+00 1.0000000E-01 -6.8211000E+01 4.2960000E+00 1.0000000E+00 1.0000000E-01 -7.6738000E+01 4.0830000E+00 1.0000000E+00 1.0000000E-01 -8.5268000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 -8.7600000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 +====== Hub Properties ============================================================================== [used only when Buoyancy=True] +0.0 VolHub - Hub volume (m^3) +0.0 HubCenBx - Hub center of buoyancy x direction offset (m) +====== Nacelle Properties ========================================================================== [used only when Buoyancy=True] +0.0 VolNac - Nacelle volume (m^3) +0,0,0 NacCenB - Position of nacelle center of buoyancy from yaw bearing in nacelle coordinates (m) +====== Tail fin Aerodynamics ======================================================================== +False TFinAero - Calculate tail fin aerodynamics model (flag) +"unused" TFinFile - Input file for tail fin aerodynamics [used only when TFinAero=True] +====== Tower Influence and Aerodynamics ============================================================ [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True] + 12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow/=0, TwrAero=True, or Buoyancy=True] +TwrElev TwrDiam TwrCd TwrTI TwrCb !TwrTI used only with TwrShadow=2, TwrCb used only with Buoyancy=True +(m) (m) (-) (-) (-) +0.0000000E+00 6.0000000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.5261000E+00 5.7870000E+00 1.0000000E+00 1.0000000E-01 0.0 +1.7053000E+01 5.5740000E+00 1.0000000E+00 1.0000000E-01 0.0 +2.5579000E+01 5.3610000E+00 1.0000000E+00 1.0000000E-01 0.0 +3.4105000E+01 5.1480000E+00 1.0000000E+00 1.0000000E-01 0.0 +4.2633000E+01 4.9350000E+00 1.0000000E+00 1.0000000E-01 0.0 +5.1158000E+01 4.7220000E+00 1.0000000E+00 1.0000000E-01 0.0 +5.9685000E+01 4.5090000E+00 1.0000000E+00 1.0000000E-01 0.0 +6.8211000E+01 4.2960000E+00 1.0000000E+00 1.0000000E-01 0.0 +7.6738000E+01 4.0830000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.5268000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 0.0 +8.7600000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 0.0 ====== Outputs ==================================================================================== True SumPrint - Generate a summary file listing input options and interpolated properties to ".AD.sum"? (flag) 7 NBlOuts - Number of blade node outputs [0 - 9] (-) diff --git a/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_ElastoDyn.dat b/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_ElastoDyn.dat index 40b6ea8f9..817400f34 100644 --- a/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_ElastoDyn.dat +++ b/reg_tests/test_files/nrel5MWactuatorLine/5MW_Baseline/NRELOffshrBsline5MW_Onshore_ElastoDyn.dat @@ -95,6 +95,11 @@ False PtfmYDOF - Platform yaw rotation DOF (flag) 0 TeetHStP - Rotor-teeter hard-stop position (degrees) [used only for 2 blades and when TeetMod=1] 0 TeetSSSp - Rotor-teeter soft-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] 0 TeetHSSp - Rotor-teeter hard-stop linear-spring constant (N-m/rad) [used only for 2 blades and when TeetMod=1] +---------------------- YAW-FRICTION -------------------------------------------- + 0 YawFrctMod - {0: none, 1: friction without Fz term at the yaw bearing, 2: friction includes Fz term at yaw bearing, 3: user defined model} (switch) + 300 M_CSmax - Maximum Coulomb friction torque (N-m)[mu_s*D_eff when YawFrctMod=1 and Fz*mu_s*D_eff when YawFrctMod=2] + 40 M_CD - Dynamic friction moment at null yaw rate (N-m) [mu_d*D_eff when YawFrctMod=1 and Fz*mu_d*D_eff when YawFrctMod=2] + 0 sig_v - Viscous friction coefficient (N-m/(rad/s)) ---------------------- DRIVETRAIN ---------------------------------------------- 100 GBoxEff - Gearbox efficiency (%) 97 GBRatio - Gearbox ratio (-)