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authorblendoit <blendoit@gmail.com>2019-10-04 11:47:39 -0700
committerblendoit <blendoit@gmail.com>2019-10-04 11:47:39 -0700
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#+TITLE: Aircraft Studio
#+AUTHOR: Marius Peter
+#+EMAIL: mpeter@ucla.edu
This program enables the creation of NACA airfoils;
the analysis of the airfoil's structural properties;
@@ -7,3 +8,26 @@ the optimization via genetic algorithm of a population of airfoils;
With the final objective of designing a lightweight FAR 23 compliant airfoil.
I adapted it from my own code for the UCLA MAE 154B final project (Spring 2019).
+
+* Program Structure
+
+** =creator.py=
+ This module enables the creation of discrete aircraft components.
+
+** =evaluator.py=
+
+** =generator.py=
+ The =generator= module contains classes describing aircrafts comprised
+ of sufficient =creator= components that they can be fed to the =evaluator=
+ for useful analysis.
+
+* Program Flow
+
+ 1. Create an =evaluator= object
+ 2. Populate the =evaluator= with aircrafts by either:
+ 1. Using =generator= methods to create an aircraft from a template
+ 2. Using =creator= to manually describe all aircraft components
+ 3. Use =evaluator= methods to:
+ 1. Calculate relevant aircraft properties
+ 2. Set desired optimization parameter(s)
+ 3. Execute the genetic algoritm and return an optimized aircraft
Copyright 2019--2024 Marius PETER