lint errors

convexengineering · Nov 16, 2017 · 9e017e2 · 9e017e2
1 parent 691ff0e
commit 9e017e2
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Showing 4 changed files with 6 additions and 5 deletions.
diff --git a/gpkitmodels/GP/aircraft/tail/tail_aero.py b/gpkitmodels/GP/aircraft/tail/tail_aero.py
@@ -38,7 +38,7 @@ def setup(self, static, state):
             orient="records")[0]
 
         constraints = [
-            Re == (V*rho*S/b/mu),
+            Re == V*rho*S/b/mu,
             # XfoilFit(fd, Cd, [Re, static["\\tau"]],
             #          err_margin="RMS", airfoil="naca 0008")
             XfoilFit(fd, Cd, [Re, static.planform.tau], err_margin="RMS")

diff --git a/gpkitmodels/GP/aircraft/tail/tail_boom.py b/gpkitmodels/GP/aircraft/tail/tail_boom.py
@@ -30,7 +30,7 @@ def setup(self, static, state):
         V = self.V = state.V
         mu = self.mu = state.mu
 
-        return [Re == (V*rho*l/mu),
+        return [Re == V*rho*l/mu,
                 Cf >= 0.455/Re**0.3,
                ]
 

diff --git a/gpkitmodels/GP/aircraft/wing/wing.py b/gpkitmodels/GP/aircraft/wing/wing.py
@@ -130,7 +130,7 @@ def setup(self, static, state,
             independentvars = [self.CL, self.Re, static.planform.tau]
 
         return [Cd >= cdp + CL**2/np.pi/AR/e,
-                Re == (rho*V*cmac/mu),
+                Re == rho*V*cmac/mu,
                 # XfoilFit(fd, cdp, [CL, Re], airfoil="jho1.dat"),
                 XfoilFit(fd, cdp, independentvars),
                 CL <= CLstall

diff --git a/gpkitmodels/GP/aircraft/wing/wing_test.py b/gpkitmodels/GP/aircraft/wing/wing_test.py
@@ -1,9 +1,9 @@
 " wing test "
 from gpkitmodels.GP.aircraft.wing.wing import Wing
 from gpkitmodels.GP.aircraft.wing.boxspar import BoxSpar
-from gpkit import Variable, Model, parse_variables
+from gpkit import Model, parse_variables
 
-#pylint: disable=no-member
+#pylint: disable=no-member, exec-used
 
 class FlightState(Model):
     """ Flight State
@@ -74,6 +74,7 @@ def box_spar():
     m.solve(verbosity=0)
 
 def test():
+    " tests "
     wing_test()
     box_spar()