1 files changed, 0 insertions, 66 deletions
diff --git a/evaluator/inertia.py b/evaluator/inertia.py
deleted file mode 100644
index f047766..0000000
--- a/evaluator/inertia.py
+++ /dev/null
@@ -1,66 +0,0 @@
-def get_centroid(aircraft):
-    """Return the coordinates of the centroid."""
-    # stringer_area = aircraft.wing.stringers.area
-    # cap_area = aircraft.wing.spars.cap_area
-
-    # TODO: Fix this
-    # caps_x = [value for spar in aircraft.wing.spars.x for value in spar]
-    # caps_z = [value for spar in aircraft.wing.spars.z for value in spar]
-    # stringers_x = aircraft.wing.stringers.x
-    # stringers_z = aircraft.wing.stringers.z
-
-    # denominator = float(
-    #     len(caps_x) * cap_area + len(stringers_x) * stringer_area)
-
-    # centroid_x = float(
-    #     sum([x * cap_area
-    #          for x in caps_x]) + sum([x * stringer_area for x in stringers_x]))
-    # centroid_x = centroid_x / denominator
-
-    # centroid_z = float(
-    #     sum([z * cap_area
-    #          for z in caps_z]) + sum([z * stringer_area for z in stringers_z]))
-    # centroid_z = centroid_z / denominator
-
-    # return (centroid_x, centroid_z)
-    return (200, 420)
-
-
-def get_inertia_terms(self):
-    """Obtain all inertia terms."""
-    stringer_area = self.stringer.area
-    cap_area = self.spar.cap_area
-
-    # Adds upper and lower components' coordinates to list
-    x_stringers = self.stringer.x
-    z_stringers = self.stringer.z
-    x_spars = self.spar.x[:][0] + self.spar.x[:][1]
-    z_spars = self.spar.z[:][0] + self.spar.z[:][1]
-    stringer_count = range(len(x_stringers))
-    spar_count = range(len(self.spar.x))
-
-    # I_x is the sum of the contributions of the spar caps and stringers
-    # TODO: replace list indices with dictionary value
-    I_x = sum(
-        [cap_area * (z_spars[i] - self.centroid[1])**2 for i in spar_count])
-    I_x += sum([
-        stringer_area * (z_stringers[i] - self.centroid[1])**2
-        for i in stringer_count
-    ])
-
-    I_z = sum(
-        [cap_area * (x_spars[i] - self.centroid[0])**2 for i in spar_count])
-    I_z += sum([
-        stringer_area * (x_stringers[i] - self.centroid[0])**2
-        for i in stringer_count
-    ])
-
-    I_xz = sum([
-        cap_area * (x_spars[i] - self.centroid[0]) *
-        (z_spars[i] - self.centroid[1]) for i in spar_count
-    ])
-    I_xz += sum([
-        stringer_area * (x_stringers[i] - self.centroid[0]) *
-        (z_stringers[i] - self.centroid[1]) for i in stringer_count
-    ])
-    return (I_x, I_z, I_xz)