fixed tutorials

Author: planes

B737_AVL_Tutorial/tut_mission_B737_AVL.py

@@ -213,17 +213,8 @@ def vehicle_setup():
     wing.symmetric               = True
     wing.high_lift               = True
     wing.dynamic_pressure_ratio  = 1.0
-    
-    # ------------------------------------------------------------------
-    #   Flaps
-    # ------------------------------------------------------------------
-    wing.flaps.chord      =  0.30   # 30% of the chord
-    wing.flaps.span_start =  0.10   # 10% of the span
-    wing.flaps.span_end   =  0.75
-    wing.flaps.type       = 'double_slotted'
 
-    # add to vehicle
-    vehicle.append_component(wing)
+    vehicle.append_component(wing)    
 
     # ------------------------------------------------------------------        
     #  Horizontal Stabilizer
@@ -242,8 +233,6 @@ def vehicle_setup():
     wing.chords.tip              = .955 * Units.meter
     wing.chords.mean_aerodynamic = 8.0  * Units.meter
     wing.areas.reference         = 32.488   * Units['meters**2']  
-    wing.areas.exposed           = 199.7792 * Units['meters**2']  
-    wing.areas.wetted            = 249.724  * Units['meters**2']  
     wing.twists.root             = 3.0 * Units.degrees
     wing.twists.tip              = 3.0 * Units.degrees  
     wing.origin                  = [32.83,0,1.14] # meters
@@ -262,7 +251,7 @@ def vehicle_setup():
     wing.tag = 'vertical_stabilizer'    
 
     wing.aspect_ratio            = 1.91
-    wing.sweeps.quarter_chord    = 40. * Units.deg
+    wing.sweeps.quarter_chord    = 25. * Units.deg
     wing.thickness_to_chord      = 0.08
     wing.taper                   = 0.25
     wing.span_efficiency         = 0.9

Solar_UAV_Optimization/Procedure.py

@@ -105,8 +105,7 @@ def simple_sizing(nexus):
 
     # Resize the motor
     motor = vec.propulsors.network.motor
-    kv    = motor.speed_constant
-    motor = size_from_kv(motor, kv)    
+    motor = size_from_kv(motor)    
 
     # diff the new data
     vec.store_diff()

Solar_UAV_Optimization/Vehicles.py

@@ -52,7 +52,7 @@ def base_setup():
     #   Main Wing
     # ------------------------------------------------------------------   
 
-    wing = SUAVE.Components.Wings.Wing()
+    wing = SUAVE.Components.Wings.Main_Wing()
     wing.tag = 'main_wing'
 
     wing.areas.reference         = vehicle.reference_area
@@ -84,7 +84,7 @@ def base_setup():
     #  Horizontal Stabilizer
     # ------------------------------------------------------------------        
 
-    wing = SUAVE.Components.Wings.Wing()
+    wing = SUAVE.Components.Wings.Horizontal_Tail()
     wing.tag = 'horizontal_stabilizer'
 
     wing.aspect_ratio         = 10. 
@@ -116,7 +116,7 @@ def base_setup():
     #   Vertical Stabilizer
     # ------------------------------------------------------------------
 
-    wing = SUAVE.Components.Wings.Wing()
+    wing = SUAVE.Components.Wings.Vertical_Tail()
     wing.tag = 'vertical_stabilizer'    
 
     wing.aspect_ratio         = 10.       
@@ -181,8 +181,8 @@ def base_setup():
 
     # Component 4 the Motor
     motor = SUAVE.Components.Energy.Converters.Motor_Lo_Fid()
-    kv                         = 800. * Units['rpm/volt'] # RPM/volt is standard
-    motor                      = size_from_kv(motor, kv)    
+    motor.speed_constant       = 800. * Units['rpm/volt'] # RPM/volt is standard
+    motor                      = size_from_kv(motor)    
     motor.gear_ratio           = 1. # Gear ratio, no gearbox
     motor.gearbox_efficiency   = 1. # Gear box efficiency, no gearbox
     motor.motor_efficiency     = 0.825;