hfoil-0.1.2: Hess-Smith panel code for inviscid 2-d airfoil analysis
Numeric.HFoil.Naca4
data Naca4 a Source
Constructors
Fields
Instances
coords :: (Ord a, Floating a) => Naca4 a -> a -> ((a, a), (a, a))Source
yt :: (Ord a, Floating a) => Naca4 a -> a -> aSource
dyt :: (Ord a, Floating a) => Naca4 a -> a -> aSource
naca4 :: (Read a, Fractional a) => String -> Naca4 aSource