Merge pull request #42 from byuflowlab/remove-interpolations.jl

Remove interpolations.jl

Project.toml

@@ -4,15 +4,14 @@ authors = ["Taylor McDonnell <[email protected]", "Andrew Ning <[email protected]>"]
 version = "0.1.6"
 
 [deps]
-Interpolations = "a98d9a8b-a2ab-59e6-89dd-64a1c18fca59"
+FLOWMath = "6cb5d3fb-0fe8-4cc2-bd89-9fe0b19a99d3"
 LinearAlgebra = "37e2e46d-f89d-539d-b4ee-838fcccc9c8e"
 StaticArrays = "90137ffa-7385-5640-81b9-e52037218182"
 VSPGeom = "9b3f6a95-fce2-4bc5-94a2-f99b39986ea6"
 WriteVTK = "64499a7a-5c06-52f2-abe2-ccb03c286192"
 
 [compat]
-Interpolations = "0.13, 0.14"
 StaticArrays = "0.12, 1.0"
-WriteVTK = "1.8"
 VSPGeom = "0.6"
+WriteVTK = "1.8"
 julia = "1.5"

src/VortexLattice.jl

@@ -2,7 +2,7 @@ module VortexLattice
 
 using LinearAlgebra
 using StaticArrays
-using Interpolations
+using FLOWMath
 using WriteVTK
 using VSPGeom
 

src/geometry.jl

@@ -357,8 +357,8 @@ end
         fcore = (c, Δs) -> 1e-3,
         spacing_s = Cosine(),
         spacing_c = Uniform(),
-        interp_s = (x, y, xpt) -> linear_interpolation(x, y)(xpt),
-        interp_c = (x, y, xpt) -> linear_interpolation(x, y)(xpt))
+        interp_s = (x, y, xpt) -> FLOWMath.linear(x, y, xpt),
+        interp_c = (x, y, xpt) -> FLOWMath.linear(x, y, xpt))
 
 Discretize a potentially curved lifting surface defined by a grid with dimensions
 (3, i, j) where `i` corresponds to the chordwise direction (ordered from leading
@@ -392,8 +392,8 @@ function grid_to_surface_panels(xyz, ns, nc;
     fcore = (c, Δs) -> 1e-3,
     spacing_s = Cosine(),
     spacing_c = Uniform(),
-    interp_s = (x, y, xpt) -> linear_interpolation(x, y)(xpt),
-    interp_c = (x, y, xpt) -> linear_interpolation(x, y)(xpt))
+    interp_s = (x, y, xpt) -> FLOWMath.linear(x, y, xpt),
+    interp_c = (x, y, xpt) -> FLOWMath.linear(x, y, xpt))
 
     TF = eltype(xyz)
 
@@ -494,7 +494,7 @@ end
         fcore = (c, Δs) -> 1e-3,
         spacing_s = Cosine(),
         spacing_c = Uniform(),
-        interp_s = (x, y, xpt) -> linear_interpolation(x, y)(xpt))
+        interp_s = (x, y, xpt) -> FLOWMath.linear(x, y, xpt))
 
 Discretize a wing into `ns` spanwise and `nc` chordwise panels with associated
 vortex rings according to the spanwise discretization scheme `spacing_s` and
@@ -530,7 +530,7 @@ function wing_to_surface_panels(xle, yle, zle, chord, theta, phi, ns, nc;
     fcore = (c, Δs) -> 1e-3,
     spacing_s = Cosine(),
     spacing_c = Uniform(),
-    interp_s = (x, y, xpt) -> linear_interpolation(x, y)(xpt))
+    interp_s = (x, y, xpt) -> FLOWMath.linear(x, y, xpt))
 
     TF = promote_type(eltype(xle), eltype(yle), eltype(zle), eltype(chord), eltype(theta), eltype(phi))