minor fix for max thrust in fuel calculation

TUDelft-CNS-ATM · Apr 1, 2021 · 9f46ba3 · 9f46ba3
1 parent 9f52eb1
commit 9f46ba3
Showing 1 changed file with 1 addition and 1 deletion.
diff --git a/openap/fuel.py b/openap/fuel.py
@@ -115,7 +115,7 @@ def enroute(self, mass, tas, alt, path_angle=0):
         fuelflow = self.at_thrust(T, alt)
 
         # do not return value outside performance boundary, with a margin of 20%
-        T_max = self.thrust.climb(tas=tas, alt=alt, roc=0)
+        T_max = self.thrust.climb(tas=0, alt=alt, roc=0)
         fuelflow = np.where(T > 1.20 * T_max, np.nan, fuelflow)
 
         return fuelflow