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-rw-r--r--creator/base.py5
-rw-r--r--creator/log_base.txt0
-rw-r--r--creator/wing.py3
3 files changed, 4 insertions, 4 deletions
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
--- /dev/null
+++ b/creator/log_base.txt
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.
Copyright 2019--2024 Marius PETER