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| -rw-r--r-- | README.org | 24 | ||||
| -rw-r--r-- | creator/__init__.pyc | bin | 0 -> 311 bytes | |||
| -rw-r--r-- | doc/diagram | 5 | ||||
| -rw-r--r-- | doc/diagram.png | bin | 0 -> 5111 bytes | |||
| -rw-r--r-- | example_airfoil.py | 2 | ||||
| -rw-r--r-- | example_airfoil.pyc | bin | 0 -> 1581 bytes | |||
| -rw-r--r-- | resources/__init__.py | 0 | ||||
| -rw-r--r-- | resources/__init__.pyc | bin | 0 -> 147 bytes | |||
| -rw-r--r-- | resources/materials.pyc | bin | 0 -> 348 bytes |
9 files changed, 30 insertions, 1 deletions
@@ -1,5 +1,6 @@ #+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 diff --git a/creator/__init__.pyc b/creator/__init__.pyc Binary files differnew file mode 100644 index 0000000..022f493 --- /dev/null +++ b/creator/__init__.pyc diff --git a/doc/diagram b/doc/diagram new file mode 100644 index 0000000..6140981 --- /dev/null +++ b/doc/diagram @@ -0,0 +1,5 @@ +hide footbox +title Sequence Diagram (Footer removed) + +Alice -> Bob: Authentication Request +Bob --> Alice: Authentication Response diff --git a/doc/diagram.png b/doc/diagram.png Binary files differnew file mode 100644 index 0000000..142f1b6 --- /dev/null +++ b/doc/diagram.png diff --git a/example_airfoil.py b/example_airfoil.py index 14cf916..3488eb9 100644 --- a/example_airfoil.py +++ b/example_airfoil.py @@ -69,7 +69,7 @@ af.spar2 = creator.wing.Spar(af, 0.57, mt.aluminium) # af.stringer.info_save(SAVE_PATH, 'foo_name') # Plot components with matplotlib -# wing.plot_geom(af, [af.spar1, af.spar2], None) +# creator.wing.plot_geom(af, [af.spar1, af.spar2], None) # Evaluator object contains airfoil analysis results. eval = evaluator.Evaluator(aircraft) diff --git a/example_airfoil.pyc b/example_airfoil.pyc Binary files differnew file mode 100644 index 0000000..54505a3 --- /dev/null +++ b/example_airfoil.pyc diff --git a/resources/__init__.py b/resources/__init__.py new file mode 100644 index 0000000..e69de29 --- /dev/null +++ b/resources/__init__.py diff --git a/resources/__init__.pyc b/resources/__init__.pyc Binary files differnew file mode 100644 index 0000000..cdb6635 --- /dev/null +++ b/resources/__init__.pyc diff --git a/resources/materials.pyc b/resources/materials.pyc Binary files differnew file mode 100644 index 0000000..a6c1af9 --- /dev/null +++ b/resources/materials.pyc |
