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Merged
merged 9 commits into from
Apr 21, 2017
Merged

Moving new commits for further development on develop #5

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ade309d
fixing plot
planes May 2, 2016
ca0c140
Merge branch 'master' of https://github.com/suavecode/Tutorials
planes Jul 20, 2016
069740a
making procedure a process
planes Jul 21, 2016
c61de18
Concorde update
timdmacdo Jan 10, 2017
880772e
Concorde update 2
timdmacdo Jan 10, 2017
0007572
Merge pull request #3 from suavecode/develop
planes Jan 11, 2017
e38f004
Missing S in B737 Tutorial
planes Jan 17, 2017
59019b3
stopped running cg calculations
jmvegh Apr 21, 2017
ab8d221
removed VyPy and PyOpt imports
jmvegh Apr 21, 2017
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6 changes: 3 additions & 3 deletions Regional_Jet_Optimization/Optimize.py
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Expand Up @@ -17,14 +17,14 @@
import matplotlib.pyplot as plt
from SUAVE.Optimization import Nexus, carpet_plot
import SUAVE.Optimization.Package_Setups.scipy_setup as scipy_setup
import VyPy
import pyOpt
#import VyPy
#import pyOpt
# ----------------------------------------------------------------------
# Run the whole thing
# ----------------------------------------------------------------------
def main():
problem = setup()

output = problem.objective()
#uncomment these lines when you want to start an optimization problem from a different initial guess
'''
inputs = [1.28, 1.38]
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8 changes: 4 additions & 4 deletions Regional_Jet_Optimization/Procedure.py
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Expand Up @@ -14,8 +14,8 @@
from SUAVE.Analyses.Process import Process
from SUAVE.Methods.Propulsion.turbofan_sizing import turbofan_sizing
from SUAVE.Methods.Geometry.Two_Dimensional.Cross_Section.Propulsion.compute_turbofan_geometry import compute_turbofan_geometry
from SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity import compute_component_centers_of_gravity
from SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity import compute_aircraft_center_of_gravity
#from SUAVE.Methods.Center_of_Gravity.compute_component_centers_of_gravity import compute_component_centers_of_gravity
#from SUAVE.Methods.Center_of_Gravity.compute_aircraft_center_of_gravity import compute_aircraft_center_of_gravity
from SUAVE.Methods.Aerodynamics.Fidelity_Zero.Lift.compute_max_lift_coeff import compute_max_lift_coeff
from SUAVE.Optimization.write_optimization_outputs import write_optimization_outputs

Expand Down Expand Up @@ -204,11 +204,11 @@ def weight(nexus):
# weight analysis
weights = nexus.analyses.base.weights.evaluate()


'''
compute_component_centers_of_gravity(vehicle)
nose_load_fraction=.06
compute_aircraft_center_of_gravity(vehicle,nose_load_fraction)

'''

weights = nexus.analyses.cruise.weights.evaluate()
vehicle.mass_properties.breakdown = weights
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