delete lambda as input to wing setup for tails

convexengineering · Oct 26, 2017 · 283231f · 283231f
1 parent f45cf25
commit 283231f
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Showing 2 changed files with 5 additions and 4 deletions.
diff --git a/gpkitmodels/GP/aircraft/tail/horizontal_tail.py b/gpkitmodels/GP/aircraft/tail/horizontal_tail.py
@@ -14,8 +14,9 @@ class HorizontalTail(Wing):
     sparModel = None
 
     def setup(self, N=3, lam=0.8):
-        self.ascs = Wing.setup(self, N, lam)
-        self.planform.substitutions.update({"AR": 4, "\\tau": 0.08})
+        self.ascs = Wing.setup(self, N)
+        self.planform.substitutions.update({"AR": 4, "\\tau": 0.08,
+                                            "\\lambda": 0.8})
         self.skin.substitutions.update({"\\rho_{CFRP}": 0.049})
         self.foam.substitutions.update({"\\bar{A}_{jh01}": 0.0548,
                                         "\\rho_{foam}": 0.024})

diff --git a/gpkitmodels/GP/aircraft/tail/vertical_tail.py b/gpkitmodels/GP/aircraft/tail/vertical_tail.py
@@ -13,8 +13,8 @@ class VerticalTail(Wing):
     sparModel = None
     def setup(self, N=3, lam=0.8):
 
-        self.ascs = Wing.setup(self, N, lam)
-        self.planform.substitutions.update({"\\tau": 0.08})
+        self.ascs = Wing.setup(self, N)
+        self.planform.substitutions.update({"\\tau": 0.08, "\\lambda": 0.8})
         self.skin.substitutions.update({"\\rho_{CFRP}": 0.049})
         self.foam.substitutions.update({"\\bar{A}_{jh01}": 0.0548,
                                         "\\rho_{foam}": 0.024})