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modified text for filtCutOff description in airfoil files for OpenFAST #538 #33

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Sep 28, 2020
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modified text for filtCutOff description in airfoil files for OpenFAST #538 #33

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a7767fd
modified text for `filtCutOff` description in airfoil files
bjonkman Sep 1, 2020
4239fc0
add example AD time history file
bjonkman Sep 1, 2020
9669900
start caselist for aerodyn
bjonkman Sep 14, 2020
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2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/Cylinder1.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
3 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/Cylinder2.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
3 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/DU21_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
142 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/DU25_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
140 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/DU30_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
143 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/DU35_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
135 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/DU40_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
0.2 x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"DEFAULT" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
136 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/5MW_Baseline/Airfoils/NACA64_A17.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -46,7 +46,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
127 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AOC/Airfoils/S812_15.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
50 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AOC/Airfoils/S812_2.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
50 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AOC/Airfoils/S813_15.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
48 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AOC/Airfoils/S814_1.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
53 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AOC/Airfoils/S814_15.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
54 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_05.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_15.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_25.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_35.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_45.dat
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Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_55.dat
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Open in desktop
Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
2 changes: 1 addition & 1 deletion glue-codes/openfast/AWT27/Airfoils/AWT27_65.dat
View file
Open in desktop
Original file line number Diff line number Diff line change
Expand Up @@ -47,7 +47,7 @@ True InclUAdata ! Is unsteady aerodynamics data included in this
0 k1_hat ! Constant in the expression of Cc due to leading edge vortex effects. [ignored if UAMod<>1]
"Default" x_cp_bar ! Constant in the expression of \hat(x)_cp^v. [ignored if UAMod<>1, default = 0.2]
"Default" UACutout ! Angle of attack above which unsteady aerodynamics are disabled (deg). [Specifying the string "Default" sets UACutout to 45 degrees]
"DEFAULT" filtCutOff ! Cut-off frequency (-3 dB corner frequency) for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (Hz) [default = 20]
"DEFAULT" filtCutOff ! Reduced frequency cut-off for low-pass filtering the AoA input to UA, as well as the 1st and 2nd derivatives (-) [default = 0.5]
!........................................
! Table of aerodynamics coefficients
181 NumAlf ! Number of data lines in the following table
Expand Down
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