From ec6d5aea43382a953891313bd712b6ffc8d6668e Mon Sep 17 00:00:00 2001 From: Garrett Barter Date: Thu, 3 Mar 2022 16:39:44 -0700 Subject: [PATCH] adding new section in wrong spot --- .../IEA-15-240-RWT-Monopile_ServoDyn.dat | 10 +++++----- ...IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat | 10 +++++----- 2 files changed, 10 insertions(+), 10 deletions(-) diff --git a/OpenFAST/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat b/OpenFAST/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat index 1a98e348..d7dd56e5 100644 --- a/OpenFAST/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat +++ b/OpenFAST/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat @@ -48,11 +48,6 @@ True GenTiStp - Method to stop the generator {T: timed usin 9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s) 9999.9 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1] 9999.9 HSSBrTqF - Fully deployed HSS-brake torque (N-m) ----------------------- Aerodynamic Flow Control ------------------------------------- -0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL} -0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1] -0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1] -0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] ---------------------- NACELLE-YAW CONTROL ------------------------------------- 0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) 9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0] @@ -62,6 +57,11 @@ True GenTiStp - Method to stop the generator {T: timed usin 9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s) 0.25 YawManRat - Yaw maneuver rate (in absolute value) (deg/s) 0.0 NacYawF - Final yaw angle for override yaw maneuvers (degrees) +---------------------- Aerodynamic Flow Control ------------------------------------- +0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL} +0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1] +0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1] +0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] ---------------------- STRUCTURAL CONTROL --------------------------------------- 0 NumBStC - Number of blade structural controllers (integer) "unused" BStCfiles - Name of the file for blade tuned mass damper (quoted string) [unused when CompNTMD is false] diff --git a/OpenFAST/IEA-15-240-RWT-Monopile_wDTUcontroller/IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat b/OpenFAST/IEA-15-240-RWT-Monopile_wDTUcontroller/IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat index 4850fe4d..7c17d867 100644 --- a/OpenFAST/IEA-15-240-RWT-Monopile_wDTUcontroller/IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat +++ b/OpenFAST/IEA-15-240-RWT-Monopile_wDTUcontroller/IEA-15-240-RWT-Monopile_ServoDyn_wDTUcontroller.dat @@ -48,11 +48,6 @@ True GenTiStp - Method to stop the generator {T: timed usin 9999.9 THSSBrDp - Time to initiate deployment of the HSS brake (s) 9999.9 HSSBrDT - Time for HSS-brake to reach full deployment once initiated (sec) [used only when HSSBrMode=1] 9999.9 HSSBrTqF - Fully deployed HSS-brake torque (N-m) ----------------------- Aerodynamic Flow Control ------------------------------------- -0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL} -0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1] -0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1] -0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] ---------------------- NACELLE-YAW CONTROL ------------------------------------- 0 YCMode - Yaw control mode {0: none, 3: user-defined from routine UserYawCont, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch) 9999.9 TYCOn - Time to enable active yaw control (s) [unused when YCMode=0] @@ -62,6 +57,11 @@ True GenTiStp - Method to stop the generator {T: timed usin 9999.9 TYawManS - Time to start override yaw maneuver and end standard yaw control (s) 0.25 YawManRat - Yaw maneuver rate (in absolute value) (deg/s) 0.0 NacYawF - Final yaw angle for override yaw maneuvers (degrees) +---------------------- Aerodynamic Flow Control ------------------------------------- +0 AfCmode - Airfoil control mode {0- none, 1- cosine wave cycle, 4- user-defined from Simulink/Labview, 5- user-defined from Bladed-style DLL} +0.0 AfC_Mean - Mean level for sinusoidal cycling or steady value (-) [used only with AfCmode==1] +0.0 AfC_Amp - Amplitude for for cosine cycling of flap signal (AfC = AfC_Amp*cos(Azimuth+phase)+AfC_mean) (-) [used only with AfCmode==1] +0.0 AfC_phase - Phase relative to the blade azimuth (0 is vertical) for for cosine cycling of flap signal (deg) [used only with AfCmode==1] ---------------------- STRUCTURAL CONTROL --------------------------------------- 0 NumBStC - Number of blade structural controllers (integer) "unused" BStCfiles - Name of the file for blade tuned mass damper (quoted string) [unused when CompNTMD is false]