Skip to content

Commit

Permalink
Update Model
Browse files Browse the repository at this point in the history
  • Loading branch information
nikhar-abbas committed Sep 25, 2020
1 parent aa8a5f6 commit 7111606
Show file tree
Hide file tree
Showing 16 changed files with 206 additions and 188 deletions.
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/Cylinder1.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"Cylinder1_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/Cylinder2.dat
Original file line number Diff line number Diff line change
Expand Up @@ -7,6 +7,7 @@
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"Cylinder2_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
! ......... x-y coordinates are next if NumCoords > 0 .............
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/DU21_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"DU21_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/DU25_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"DU25_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/DU30_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"DU30_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/DU35_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"DU35_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/DU40_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"DU40_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
1 change: 1 addition & 0 deletions Test_Cases/NREL-5MW/Airfoils/NACA64_A17.dat
Original file line number Diff line number Diff line change
Expand Up @@ -6,6 +6,7 @@
"DEFAULT" InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=1]
1 NonDimArea ! The non-dimensional area of the airfoil (area/chord^2) (set to 1.0 if unsure or unneeded)
@"NACA64_A17_coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included.
"unused" BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called.
1 NumTabs ! Number of airfoil tables in this file.
! ------------------------------------------------------------------------------
! data for table 1
Expand Down
Loading

0 comments on commit 7111606

Please sign in to comment.