Fix tests

Author: ufechner7

src/VortexStepMethod.jl

@@ -20,6 +20,8 @@ using PrecompileTools
 using Pkg
 using DifferentiationInterface
 import SciMLBase: successful_retcode
+import YAML
+import Base: show
 
 # Export public interface
 export Wing, Section, RamAirWing, init!
@@ -262,6 +264,7 @@ function help(url)
 end
 
 # Include core functionality
+include("settings.jl")
 include("wing_geometry.jl")
 include("kite_geometry.jl")
 include("filament.jl")

src/settings.jl

@@ -1,16 +1,29 @@
-using Parameters
+filename = "vsm_settings.yaml"
+data = YAML.load_file(joinpath(dirname(dirname(pathof(VortexStepMethod))), "data", filename))
 
-@with_kw mutable struct WingSettings
-    n_panels::Int
-    spanwise_panel_distribution::String = "uniform"
+@Base.kwdef mutable struct WingSettings
+    name::String = "main_wing"
+    n_panels::Int64 = 40
+    n_groups::Int64 = 40 
+    spanwise_panel_distribution::String = "LINEAR"
+    spanwise_direction::MVec3 = [0.0, 1.0, 0.0]
+    remove_nan = true
 end
 
-@with_kw mutable struct VSMSettings
+@Base.kwdef mutable struct SolverSettings
     aerodynamic_model_type::String = "VSM"
-    max_iterations::Int = 1000
+    max_iterations::Int64 = 1000
 end
 
-@with_kw mutable struct Configuration
-    wings::Vector{Dict{String, WingSettings}}
-    solver_settings::VSMSettings
-end
+@Base.kwdef mutable struct VSMSettings
+    wings::Vector{WingSettings} = [WingSettings()]
+    solver_settings::SolverSettings = SolverSettings()
+end
+
+function Base.show(io::IO, vs::VSMSettings)
+    println(io, "VSMSettings:")
+    for wing in vs.wings
+        print(io, "    ", replace(repr(wing), "\n" => "\n    "))
+    end
+    print(io, replace(repr(vs.solver_settings), "\n" => "\n    "))
+end