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Merge pull request OpenFAST#11 from andrew-platt/MDv2-farm into matte…
…hall/MDv2-farm Update to OpenFAST/dev branch, and some SrvD_Linearization updates
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Original file line number | Diff line number | Diff line change |
---|---|---|
@@ -1,12 +1,12 @@ | ||
! ------------ AirfoilInfo v1.01.x Input File ---------------------------------- | ||
! ------------ AirfoilInfo Input File ------------------------------------------ | ||
! AeroElasticSE FAST driver | ||
! | ||
! | ||
! ------------------------------------------------------------------------------ | ||
DEFAULT InterpOrd ! Interpolation order to use for quasi-steady table lookup {1=linear; 3=cubic spline; "default"} [default=3] | ||
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) | ||
@"AF20_Coords.txt" NumCoords ! The number of coordinates in the airfoil shape file. Set to zero if coordinates not included. | ||
AF20_BL.txt BL_file ! The file name including the boundary layer characteristics of the profile. Ignored if the aeroacoustic module is not called. | ||
AF20_BL.txt BL_file ! The file name including the boundary layer characteristics of the profile. Optional and ignored if the aeroacoustic module is not called. | ||
1 NumTabs ! Number of airfoil tables in this file. Each table must have lines for Re and Ctrl. | ||
! ------------------------------------------------------------------------------ | ||
! data for table 1 |
4 changes: 2 additions & 2 deletions
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docs/source/user/aerodyn-aeroacoustics/example/AeroAcousticsInput.dat
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