hfoil-0.1.2: Hess-Smith panel code for inviscid 2-d airfoil analysis
Numeric.HFoil.Foil
data Foil a Source
Constructors
Instances
data Element a Source
Fields
panelizeNaca4 :: (Enum a, Floating (Vector a), RealFloat a, Field a) => Naca4 a -> Int -> Foil aSource
loadFoil :: FilePath -> IO (Either String (Foil Double))Source
getUIUCFoil :: (Num (Vector a), Read a, RealFloat a, Container Vector a) => String -> IO (Either String (Foil a))Source