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-rw-r--r--creator/wing.py4
1 files changed, 2 insertions, 2 deletions
diff --git a/creator/wing.py b/creator/wing.py
index 59f5bbe..cc7d29a 100644
--- a/creator/wing.py
+++ b/creator/wing.py
@@ -24,7 +24,7 @@ import resources.materials as mt
class Airfoil(base.Component):
"""This class represents a single NACA airfoil.
- The coordinates are saved as two lists
+ The coordinates are saved as two np.arrays
for the x- and z-coordinates. The coordinates start at
the leading edge, travel over the airfoil's upper edge,
then loop back to the leading edge via the lower edge.
@@ -141,9 +141,9 @@ class Spar(base.Component):
super().__init__(parent, name)
super().set_material(material)
self.cap_area = float()
- loc = loc_percent * parent.chord
# bi.bisect_left: returns index of first value in parent.x > loc
# This ensures that spar geom intersects with airfoil geom.
+ loc = loc_percent * parent.chord
# Spar upper coordinates
spar_u = bi.bisect_left(parent.x, loc) - 1
self.x = np.append(self.x, parent.x[spar_u])
Copyright 2019--2024 Marius PETER