Some progress

Author: ufechner7

data/vsm_settings.yaml

@@ -1,9 +1,10 @@
 wings:
     - main_wing:
         n_panels: 40
-        spanwise_panel_distribution: "uniform"
+        spanwise_panel_distribution: "LINEAR"
+        spanwise_direction: [0.0, 1.0, 0.0]
     - tail:
         n_panels: 20
 solver_settings:
-    aerodynamic_model_type:
-    max_iterations:
+    aerodynamic_model_type: "VSM"
+    max_iterations: 1000

mwes/mwe_04.jl

@@ -1,7 +1,25 @@
 # read the vsm_settings.yaml file
 
 import YAML
+using Parameters
 
 filename = "vsm_settings.yaml"
 data = YAML.load_file(joinpath("data", filename))
 
+@with_kw mutable struct WingSettings
+    name::String = "main_wing"
+    n_groups::Int64 = 40 
+    n_panels::Int64 = 40
+    spanwise_panel_distribution::String = "LINEAR"
+end
+
+@with_kw mutable struct SolverSettings
+    aerodynamic_model_type::String = "VSM"
+    max_iterations::Int64 = 1000
+end
+
+@with_kw mutable struct VSMSettings
+    wings::Vector{WingSettings} = [WingSettings()]
+    solver_settings::SolverSettings = SolverSettings()
+end
+

src/settings.jl

@@ -0,0 +1,16 @@
+using Parameters
+
+@with_kw mutable struct WingSettings
+    n_panels::Int
+    spanwise_panel_distribution::String = "uniform"
+end
+
+@with_kw mutable struct VSMSettings
+    aerodynamic_model_type::String = "VSM"
+    max_iterations::Int = 1000
+end
+
+@with_kw mutable struct Configuration
+    wings::Vector{Dict{String, WingSettings}}
+    solver_settings::VSMSettings
+end