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1 change: 0 additions & 1 deletion aviary/docs/examples_unreviewed/modified_aircraft.csv
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Expand Up @@ -52,7 +52,6 @@ aircraft:engine:reference_mass,7400,lbm
aircraft:engine:reference_sls_thrust,28928.1,lbf
aircraft:engine:scale_factor,1.0,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,28928.1,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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Expand Up @@ -158,7 +158,6 @@
"Aircraft.Engine = Aircraft.Engine\n",
"check_contains(required_options, CoreMetaData)\n",
"required = ( # f'{Aircraft.Engine.DATA_FILE=}'.split('=')[0],\n",
" get_variable_name(Aircraft.Engine.SCALE_PERFORMANCE),\n",
" get_variable_name(Aircraft.Engine.IGNORE_NEGATIVE_THRUST),\n",
" get_variable_name(Aircraft.Engine.GEOPOTENTIAL_ALT),\n",
" get_variable_name(Aircraft.Engine.GENERATE_FLIGHT_IDLE),\n",
Expand Down Expand Up @@ -213,7 +212,7 @@
"If you are missing any required variables, you may see a warning at runtime, depending on verbosity level. Aviary will try using the default value for the missing variable, which may affect analysis results.\n",
"\n",
"```\n",
"UserWarning: <aircraft:engine:scale_performance> is a required option for EngineDecks, but has not been specified for EngineDeck <example>. The default value will be used.\n",
"UserWarning: <aircraft:engine:generate_flight_idle> is a required option for EngineDecks, but has not been specified for EngineDeck <example>. The default value will be used.\n",
"```\n",
"\n",
"<!-- See !!!LINK HERE!!! for a complete list of all available options to define engine behavior -->\n",
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8 changes: 0 additions & 8 deletions aviary/interface/test/sizing_results_for_test.json
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Expand Up @@ -407,14 +407,6 @@
"unitless",
"<class 'list'>"
],
[
"aircraft:engine:scale_performance",
[
true
],
"unitless",
"<class 'list'>"
],
[
"aircraft:engine:scaled_sls_thrust",
[
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Original file line number Diff line number Diff line change
Expand Up @@ -213,7 +213,6 @@
inputs.set_val(Aircraft.Engine.WING_LOCATIONS, 0.289682918)
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0)
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Expand Up @@ -72,7 +72,6 @@ aircraft:engine:reference_mass,22017.0,lbm
aircraft:engine:reference_sls_thrust,86459.2,lbf
aircraft:engine:scale_factor,0.8096304384,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,70000,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.0,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.0,unitless
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Expand Up @@ -167,7 +167,6 @@
inputs.set_val(Aircraft.Engine.SCALE_FACTOR, 0.8096304384) # THRUST/THRSO
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.0) # EEXP
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0) # FFFSUB
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0) # FFFSUP
inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0) # DFFAC
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Expand Up @@ -72,7 +72,6 @@ aircraft:engine:reference_mass,22017.0,lbm
aircraft:engine:reference_sls_thrust,86459.2,lbf
aircraft:engine:scale_factor,0.8096304384,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,70000,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.0,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.0,unitless
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Expand Up @@ -169,7 +169,6 @@
inputs.set_val(Aircraft.Engine.SCALE_FACTOR, 0.8096304384) # THRUST/THRSO
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.0) # EEXP
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0) # FFFSUB
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0) # FFFSUP
inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0) # DFFAC
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Original file line number Diff line number Diff line change
Expand Up @@ -162,7 +162,6 @@
inputs.set_val(Aircraft.Engine.SCALE_FACTOR, 1.0)
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0)
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Original file line number Diff line number Diff line change
Expand Up @@ -168,7 +168,6 @@
inputs.set_val(Aircraft.Engine.THRUST_REVERSERS_MASS_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SCALE_FACTOR, 1.0)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
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Expand Up @@ -167,7 +167,6 @@
inputs.set_val(Aircraft.Engine.THRUST_REVERSERS_MASS_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)

inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
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Expand Up @@ -158,7 +158,6 @@
inputs.set_val(Aircraft.Engine.THRUST_REVERSERS_MASS_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0)
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Expand Up @@ -164,7 +164,6 @@
engine_1_inputs.set_val(Aircraft.Engine.WING_LOCATIONS, 15.8300 / (117.83 / 2))
engine_1_inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
engine_1_inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
engine_1_inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
engine_1_inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
engine_1_inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
engine_1_inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0)
Expand Down Expand Up @@ -197,7 +196,6 @@
engine_2_inputs.set_val(Aircraft.Engine.WING_LOCATIONS, 0.289682918)
engine_2_inputs.set_val(Aircraft.Engine.SCALE_MASS, True)
engine_2_inputs.set_val(Aircraft.Engine.MASS_SCALER, 1.15)
engine_2_inputs.set_val(Aircraft.Engine.SCALE_PERFORMANCE, True)
engine_2_inputs.set_val(Aircraft.Engine.SUBSONIC_FUEL_FLOW_SCALER, 1.0)
engine_2_inputs.set_val(Aircraft.Engine.SUPERSONIC_FUEL_FLOW_SCALER, 1.0)
engine_2_inputs.set_val(Aircraft.Engine.FUEL_FLOW_SCALER_CONSTANT_TERM, 0.0)
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Original file line number Diff line number Diff line change
Expand Up @@ -52,7 +52,6 @@ aircraft:engine:reference_mass,7400,lbm
aircraft:engine:reference_sls_thrust,28928.1,lbf
aircraft:engine:scale_factor,1.0,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,28928.1,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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Original file line number Diff line number Diff line change
Expand Up @@ -51,7 +51,6 @@ aircraft:engine:reference_mass,7400,lbm
aircraft:engine:reference_sls_thrust,28928.1,lbf
aircraft:engine:scale_factor,1.0,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,28928.1,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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Expand Up @@ -17,7 +17,6 @@ aircraft:design:drag_divergence_shift,0.033,unitless
aircraft:engine:constant_fuel_consumption,0.,lbm/h
aircraft:engine:data_file,models/engines/turbofan_23k_1.csv,unitless
aircraft:engine:global_throttle, True, unitless
aircraft:engine:scale_performance,False,unitless
aircraft:engine:mass_specific,0.21366,lbm/lbf
aircraft:engine:fuel_flow_scaler_constant_term,0.,unitless
aircraft:engine:fuel_flow_scaler_linear_term,0.,unitless
Expand All @@ -37,7 +36,6 @@ aircraft:engine:reference_mass,7400,lbm
aircraft:engine:reference_sls_thrust,28928.1,lbf
aircraft:engine:scale_factor,1.0,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,28928.1,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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Original file line number Diff line number Diff line change
Expand Up @@ -51,7 +51,6 @@ aircraft:engine:reference_mass,7400,lbm
aircraft:engine:reference_sls_thrust,28928.1,lbf
aircraft:engine:scale_factor,1.0,unitless
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,28928.1,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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Expand Up @@ -44,7 +44,6 @@ aircraft:engine:num_wing_engines,2,unitless
aircraft:engine:reference_mass,4600.0,lbm
aircraft:engine:reference_sls_thrust,23000.0,lbf
aircraft:engine:scale_mass,True,unitless
aircraft:engine:scale_performance,True,unitless
aircraft:engine:scaled_sls_thrust,23000.0,lbf
aircraft:engine:subsonic_fuel_flow_scaler,1.,unitless
aircraft:engine:supersonic_fuel_flow_scaler,1.,unitless
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