delete unnecessary imports; add lines to EOF; fix variable descrp typo

convexengineering · Oct 16, 2017 · a0e73f0 · a0e73f0
1 parent 1f55f19
commit a0e73f0
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Showing 4 changed files with 9 additions and 13 deletions.
diff --git a/gpkitmodels/GP/aircraft/tail/horizontal_tail.py b/gpkitmodels/GP/aircraft/tail/horizontal_tail.py
@@ -1,14 +1,10 @@
 " horizontal tail "
 import numpy as np
-from gpkit import Model, Variable
+from gpkit import Variable
 from .tail_aero import TailAero
 from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.wing.constant_taper_chord import c_bar
-from gpkitmodels.GP.aircraft.wing.wing_interior import WingInterior
-from gpkitmodels.GP.aircraft.wing.wing_skin import WingSkin
 
-#pylint: disable=invalid-name, too-many-locals, unused-variable
-#pylint: disable=attribute-defined-outside-init
+#pylint: disable=attribute-defined-outside-init, unused-variable
 
 class HorizontalTail(Wing):
     "horizontal tail model"
@@ -28,3 +24,4 @@ def setup(self, N=3, lam=0.8):
         mh = Variable("m_h", "-", "horizontal tail span effectiveness")
 
         return self.ascs, mh*(1+2.0/self.planform["AR"]) <= 2*np.pi
+
diff --git a/gpkitmodels/GP/aircraft/tail/vertical_tail.py b/gpkitmodels/GP/aircraft/tail/vertical_tail.py
@@ -1,13 +1,9 @@
 " vertical tail "
-from gpkit import Model, Variable
+from gpkit import Variable
 from .tail_aero import TailAero
 from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.wing.constant_taper_chord import c_bar
-from gpkitmodels.GP.aircraft.wing.wing_interior import WingInterior
-from gpkitmodels.GP.aircraft.wing.wing_skin import WingSkin
 
-#pylint: disable=invalid-name, too-many-locals, unused-variable
-#pylint: disable=attribute-defined-outside-init
+#pylint: disable=attribute-defined-outside-init, unused-variable
 
 class VerticalTail(Wing):
     "vertical tail model"
@@ -25,3 +21,4 @@ def setup(self, N=3, lam=0.8):
         lv = Variable("l_v", "ft", "vertical tail moment arm")
 
         return self.ascs, self.components
+
diff --git a/gpkitmodels/GP/aircraft/wing/constant_taper_chord.py b/gpkitmodels/GP/aircraft/wing/constant_taper_chord.py
@@ -8,3 +8,4 @@ def c_bar(lam, N):
     cbarmac = 2./3*(1+lam+lam**2)/(1+lam)
     deta = np.diff(eta)
     return c, eta, deta, cbarmac
+
diff --git a/gpkitmodels/GP/aircraft/wing/wing.py b/gpkitmodels/GP/aircraft/wing/wing.py
@@ -36,7 +36,7 @@ def setup(self, N):
             cbave = Variable("\\bar{c}_{ave}", "-",
                              "normalized mid section chord")
             cave = Variable("c_{ave}", "ft", "mid section chord")
-            deta = Variable("d\\eta", "-", "\\Detla (2y/b)")
+            deta = Variable("d\\eta", "-", "\\Delta (2y/b)")
 
         constraints = [b**2 == S*AR,
                        cave == cbave*S/b,
@@ -127,3 +127,4 @@ def setup(self, N=5, lam=0.5):
         constraints = [W/mfac >= sum(c["W"] for c in self.components)]
 
         return constraints, self.planform, self.components
+