Minor fixes.

fast-aircraft-design · Apr 26, 2023 · 0939b08 · 0939b08
1 parent 568aedd
commit 0939b08
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Showing 3 changed files with 10 additions and 10 deletions.
diff --git a/docs/documentation/mission_module/mission_file/segments.rst b/docs/documentation/mission_module/mission_file/segments.rst
@@ -526,11 +526,11 @@ The parameters for this segment are the same as for its 3 components, except tha
     segment: takeoff
     wheels_friction: 0.03
     rotation_equivalent_airspeed:
-        value: data:mission:operational:takeoff:Vr
+      value: data:mission:operational:takeoff:Vr
     rotation_rate:
       value: 0.0523
-      units: rad
-    rotation_alpha_limit_truc:
+      units: rad/s
+    rotation_alpha_limit:
       value: 0.3489
       units: rad
     end_time_step: 0.05

diff --git a/src/fastoad/models/performances/mission/openmdao/tests/data/test_mission_takeoff.yml b/src/fastoad/models/performances/mission/openmdao/tests/data/test_mission_takeoff.yml
@@ -31,7 +31,7 @@ phases:
         landing_gear_height:
           value: data:geometry:landing_gear:height
           unit: m
-        induced_drag_coef:
+        induced_drag_coefficient:
           value: data:aerodynamics:aircraft:low_speed:induced_drag_coefficient
         k_winglet:
           value: tuning:aerodynamics:aircraft:cruise:CD:winglet_effect:k
@@ -67,11 +67,11 @@ phases:
       - segment: takeoff
         wheels_friction: 0.03
         rotation_equivalent_airspeed:
-            value: data:mission:operational:takeoff:Vr
+          value: data:mission:operational:takeoff:Vr
         rotation_rate:
           value: 0.0523
-          units: rad
-        rotation_alpha_limit_truc:
+          units: rad/s
+        rotation_alpha_limit:
           value: 0.3489
           units: rad
         end_time_step: 0.05
@@ -93,7 +93,7 @@ phases:
         landing_gear_height:
           value: data:geometry:landing_gear:height
           unit: m
-        induced_drag_coef:
+        induced_drag_coefficient:
           value: data:aerodynamics:aircraft:low_speed:induced_drag_coefficient
         k_winglet:
           value: tuning:aerodynamics:aircraft:cruise:CD:winglet_effect:k

diff --git a/src/fastoad/models/performances/mission/polar_modifier.py b/src/fastoad/models/performances/mission/polar_modifier.py
@@ -83,7 +83,7 @@ class GroundEffectRaymer(AbstractPolarModifier):
     landing_gear_height: float
 
     #: Induced drag coefficient, multiplies CL**2 to obtain the induced drag
-    induced_drag_coef: float
+    induced_drag_coefficient: float
 
     #: Winglet effect tuning coefficient
     k_winglet: float
@@ -112,7 +112,7 @@ def modify_polar(self, polar: Polar, flight_point: FlightPoint) -> Polar:
         ) / self.span
         k_ground = 33.0 * h_b ** 1.5 / (1 + 33.0 * h_b ** 1.5)
         cd_ground = (
-            self.induced_drag_coef
+            self.induced_drag_coefficient
             * polar.definition_cl ** 2
             * self.k_winglet
             * self.k_cd