hfoil-0.2.0.2: Hess-Smith panel code for inviscid 2-d airfoil analysis
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 a Source
loadFoil :: FilePath -> IO (Either String (Foil Double)) Source
getUIUCFoil :: String -> IO (Either String (Foil Double)) Source