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authorMarius Peter <blendoit@gmail.com>2019-06-23 15:38:04 -0700
committerMarius Peter <blendoit@gmail.com>2019-06-23 15:38:04 -0700
commit8d6a7e582479a6fc4e0b527c39773cd2d4858faf (patch)
treedc547a388a5c7c2104f6fa7637ca1e217c055e52
parentf3c4b943012397cf085a67580acf660fe9ef7df5 (diff)
top stringer amount
-rw-r--r--main.py6
1 files changed, 3 insertions, 3 deletions
diff --git a/main.py b/main.py
index f11bd0f..b2f67a3 100644
--- a/main.py
+++ b/main.py
@@ -24,7 +24,7 @@ start_time = time.time()
# Airfoil dimensions
NACA_NUM = 2412
-CHORD_LENGTH = 101
+CHORD_LENGTH = 100
SEMI_SPAN = 40
# Airfoil thickness
@@ -37,11 +37,11 @@ SPAR_MASS = 10 # lbs
STRINGER_MASS = 5 # lbs
# Area
-SPAR_CAP_AREA = 0.0 # sqin
+SPAR_CAP_AREA = 0.3 # sqin
STRINGER_AREA = 0.1 # sqin
# Amount of stringers
-TOP_STRINGERS = 3
+TOP_STRINGERS = 6
BOTTOM_STRINGERS = 4
NOSE_TOP_STRINGERS = 3
NOSE_BOTTOM_STRINGERS = 6
Copyright 2019--2024 Marius PETER