diff options
| -rw-r--r-- | main.py | 6 |
1 files changed, 3 insertions, 3 deletions
@@ -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 |