IO bomb:

Project.toml

@@ -5,18 +5,23 @@ version = "1.0.0-DEV"
 
 [deps]
 BenchmarkTools = "6e4b80f9-dd63-53aa-95a3-0cdb28fa8baf"
+CSV = "336ed68f-0bac-5ca0-87d4-7b16caf5d00b"
 Dates = "ade2ca70-3891-5945-98fb-dc099432e06a"
+DelimitedFiles = "8bb1440f-4735-579b-a4ab-409b98df4dab"
 Dierckx = "39dd38d3-220a-591b-8e3c-4c3a8c710a94"
 DocStringExtensions = "ffbed154-4ef7-542d-bbb7-c09d3a79fcae"
 ForwardDiff = "f6369f11-7733-5829-9624-2563aa707210"
 LinearAlgebra = "37e2e46d-f89d-539d-b4ee-838fcccc9c8e"
 NLopt = "76087f3c-5699-56af-9a33-bf431cd00edd"
 NLsolve = "2774e3e8-f4cf-5e23-947b-6d7e65073b56"
+Parameters = "d96e819e-fc66-5662-9728-84c9c7592b0a"
 Printf = "de0858da-6303-5e67-8744-51eddeeeb8d7"
 PyPlot = "d330b81b-6aea-500a-939a-2ce795aea3ee"
+Revise = "295af30f-e4ad-537b-8983-00126c2a3abe"
 Roots = "f2b01f46-fcfa-551c-844a-d8ac1e96c665"
 StaticArrays = "90137ffa-7385-5640-81b9-e52037218182"
 TOML = "fa267f1f-6049-4f14-aa54-33bafae1ed76"
+Tables = "bd369af6-aec1-5ad0-b16a-f7cc5008161c"
 Test = "8dfed614-e22c-5e08-85e1-65c5234f0b40"
 Trapz = "592b5752-818d-11e9-1e9a-2b8ca4a44cd1"
 Zygote = "e88e6eb3-aa80-5325-afca-941959d7151f"

docs/make.jl

@@ -40,6 +40,8 @@ makedocs(
         "sizing/sizing.md",
         "sizing/weightmodels.md"
         ],
+    "Data and I/O" => "data_io/data_io.md",
+
     "Miscellaneous" => Any[
         "misc/structs.md",
         "misc/dreladocs.md",

docs/src/data_io/data_io.md

@@ -0,0 +1,36 @@
+
+---
+# Data structure basics
+
+## `aircraft` struct
+
+## `par` arrays
+
+Refer to the [struct reference page](@ref datastructs) for add'l details.
+
+---
+# Inputting to models
+
+## `.toml`s and the default input
+tweak default input or import then tweak for example, to _____
+
+```julia
+igTmetal = 239 #index for max metal temp (see src/misc/index.inc)
+ac = load_default_model() #creates new aircraft using default input .toml
+ac.parg[igTmetal] = 2000 #set max metal temp to 2000 K
+```
+
+## Reading externals
+
+temp
+
+
+---
+
+# Exporting from models
+
+## Quicksave and quickload via .toml
+
+## Saving model to a readable .toml
+
+## Output data to .csv

example/example_TF_run.jl

@@ -14,17 +14,19 @@ include("../tasopt.jl")
 include("737input.jl")
 
 # 3) Size aircraft
-saveOD = false
-time_wsize = @elapsed size_aircraft(35, 0, false, true, saveOD)
+time_wsize = @elapsed size_aircraft(iter=35, initwgt=false, 
+                                    Ldebug=false, printiter=true, 
+                                    saveOD=false)
 println(parg[igWMTO])
 
 # 4) Visualize outputs
 # Output resulting geometry of aircraft
 geometry(parg)
 
 
-# Show weight buildup of the aircraft
-weight_buildup(parg)
+
+# # Show weight buildup of the aircraft
+# weight_buildup(parg)
 
 # 5) Plot figures
 pygui(true)

example/example_drela_run.jl

@@ -8,17 +8,17 @@ using TASOPT
 include("737input_2.jl")
 
 # 3) Size aircraft
-time_wsize = @elapsed size_aircraft(B737, 35, 0, false, true, saveOD)
+time_wsize = @elapsed size_aircraft!(B737)
 println("Time to size aircraft = $time_wsize s")
 
 # 4) Visualize outputs
 # Output resulting geometry of aircraft
-TASOPT.geometry(B737.parg)
+# TASOPT.geometry(B737.parg) #TODO: needs update to use
 
 # Show weight buildup of the aircraft
-TASOPT.weight_buildup(B737.parg)
+# TASOPT.weight_buildup(B737.parg) #TODO: needs update to use
 
 # 5) Plot figures
-pygui(true)
-stickfig(parg, pari, parm)
+# pygui(true) #TODO: needs update to use (this and below)
+# stickfig(parg, pari, parm)
 # plt.savefig("../../example/Example.png") # BUG