From 1e8f2782753d70da35c2122f6d4441f94ee94ed6 Mon Sep 17 00:00:00 2001 From: blendoit Date: Mon, 7 Oct 2019 21:14:10 -0700 Subject: Subcomponent tree and Evaluator analysis Made very good progress on component tree representation, and Evaluator analysis method. --- creator/base.py | 5 ++++- creator/log_base.txt | 0 creator/wing.py | 3 --- 3 files changed, 4 insertions(+), 4 deletions(-) create mode 100644 creator/log_base.txt (limited to 'creator') diff --git a/creator/base.py b/creator/base.py index 33ea680..4a794b7 100644 --- a/creator/base.py +++ b/creator/base.py @@ -5,7 +5,7 @@ import sys import os.path import logging -logging.basicConfig(filename='log.txt', +logging.basicConfig(filename='log_base.txt', level=logging.DEBUG, format='%(asctime)s - %(levelname)s - %(message)s') @@ -34,6 +34,9 @@ class Component: self.material = None self.mass = float() + def __str__(self): + return self.name + def info_print(self, round): """Print all the component's coordinates to the terminal.""" name = f' CREATOR DATA FOR {str(self).upper()} ' diff --git a/creator/log_base.txt b/creator/log_base.txt new file mode 100644 index 0000000..e69de29 diff --git a/creator/wing.py b/creator/wing.py index b21a68c..7bf0b23 100644 --- a/creator/wing.py +++ b/creator/wing.py @@ -52,9 +52,6 @@ class Airfoil(base.Component): self.spars = [] self.stringers = [] - def __str__(self): - return self.name - def add_naca(self, naca_num=2412): """Generate surface geometry for a NACA airfoil. -- cgit v1.2.3