def the_aircraft_function(vehicle,mission):
# start the results data structure
results = Data()
# evaluate weights
results = evaluate_weights(vehicle,results)
# evaluate field length
results = evaluate_field_length(vehicle,mission,results)
# evaluate the mission
results = evaluate_mission(vehicle,mission,results)
# evaluate noise
results = evaluate_noise(vehicle,mission,results)
# compile results
results = compile_results(vehicle,mission,results)
return results
def the_aircraft_function(vehicle, mission):
# start the results data structure
results = Data()
# evaluate weights
results = evaluate_weights(vehicle, results)
# evaluate field length
results = evaluate_field_length(vehicle, mission, results)
# evaluate the mission
results = evaluate_mission(vehicle, mission, results)
# evaluate noise
results = evaluate_noise(vehicle, mission, results)
# compile results
results = compile_results(vehicle, mission, results)
return results
def the_aircraft_function_EMBRAER(vehicle,mission):
# start the results data structure
results = Data()
# evaluate weights
print ' Estimating weights'
results = evaluate_weights(vehicle,results)
# evaluate field length
print ' Evaluate field length'
results = evaluate_field_length(vehicle,mission,results)
# evaluate range for required payload
print ' Evaluate range for required payload'
results = evaluate_range_for_design_payload(vehicle,mission,results)
# evaluate range from short field
print ' Evaluate range from short field'
results = evaluate_range_from_short_field(vehicle,mission,results)
# evaluate design mission for fuel consuption
print ' Evaluate design mission for fuel consuption'
results = evaluate_mission_for_fuel(vehicle,mission,results)
# evaluate noise
print ' Evaluate noise'
results = evaluate_noise(vehicle,mission,results)
# compile results
results = compile_results(vehicle,mission,results)
print results.field_length
print results.design_payload_mission
print results.short_field
print results.mission_for_fuel
return results
def evaluate_noise(vehicle,mission,results):
# unpack
from SUAVE.Methods.Noise.Correlations import shevell as evaluate_noise
mission_profile = results.mission_profile
weight_landing = mission_profile.segments[-1].conditions.weights.total_mass[-1,0]
number_of_engines = vehicle.propulsors['turbo_fan'].number_of_engines
thrust_sea_level = vehicle.propulsors['turbo_fan'].thrust.design
thrust_landing = mission_profile.segments[-1].conditions.frames.body.thrust_force_vector[-1,0]
# evaluate
noise = evaluate_noise( weight_landing ,
number_of_engines ,
thrust_sea_level ,
thrust_landing )
# pack
results.noise = noise
return results
def evaluate_noise(vehicle, mission, results):
# unpack
from SUAVE.Methods.Noise.Correlations import shevell as evaluate_noise
mission_profile = results.mission_profile
weight_landing = mission_profile.segments[
-1].conditions.weights.total_mass[-1, 0]
number_of_engines = vehicle.propulsors['Turbo Fan'].number_of_engines
thrust_sea_level = vehicle.propulsors['Turbo Fan'].thrust.design
thrust_landing = mission_profile.segments[
-1].conditions.frames.body.thrust_force_vector[-1, 0]
# evaluate
noise = evaluate_noise(weight_landing, number_of_engines, thrust_sea_level,
thrust_landing)
# pack
results.noise = noise
return results
def the_aircraft_function_EMBRAER(vehicle,mission):
# start the results data structure
results = Data()
# evaluate weights
#print ' Estimating weights'
results = evaluate_weights(vehicle,results)
# evaluate field length
#print ' Evaluate field length'
results = evaluate_field_length(vehicle,mission,results)
# evaluate range for required payload
#print ' Evaluate range for required payload'
results = evaluate_range_for_design_payload(vehicle,mission,results)
# evaluate range from short field
#print ' Evaluate range from short field'
results = evaluate_range_from_short_field(vehicle,mission,results)
# evaluate design mission for fuel consuption
#print ' Evaluate design mission for fuel consuption'
results = evaluate_mission_for_fuel(vehicle,mission,results)
# evaluate noise
#print ' Evaluate noise'
results = evaluate_noise(vehicle,mission,results)
# compile results
results = compile_results(vehicle,mission,results)
#print results.field_length
#print results.design_payload_mission
#print results.short_field
#print results.mission_for_fuel
return results