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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,256 @@ | ||
| { | ||
| "$schema": "https://raw.githubusercontent.com/marioarbras/aircraft-design-tool/master/schemas/project.json", | ||
| "concept": { | ||
| "categories": { | ||
| "name": "New Concept", | ||
| "pairs": [ | ||
| [1, 0.14286], | ||
| [7, 1] | ||
| ], | ||
| "categories": [ | ||
| { | ||
| "name": "Number of Passengers", | ||
| "pairs": [ | ||
| [ 1, 0.11111, 9], | ||
| [ 9, 1, 0.11111], | ||
| [0.11111, 9, 1] | ||
| ] | ||
| }, | ||
| { | ||
| "name": "Powerplant", | ||
| "pairs": [ | ||
| [1, 0.125], | ||
| [8, 1] | ||
| ], | ||
| "categories": [ | ||
| { | ||
| "name": "Max Power Installed", | ||
| "pairs": [ | ||
| [ 1, 0.14286, 9], | ||
| [ 7, 1, 9], | ||
| [0.11111, 0.11111, 1] | ||
| ] | ||
| }, | ||
| { | ||
| "name": "Pollutant Emissions", | ||
| "pairs": [ | ||
| [ 1, 4, 0.11111], | ||
| [0.25, 1, 0.11111], | ||
| [ 9, 9, 1] | ||
| ] | ||
| } | ||
| ] | ||
| } | ||
| ] | ||
| }, | ||
| "designs": [ | ||
| { | ||
| "name": "Helicopter" | ||
| }, | ||
| { | ||
| "name": "Aircraft" | ||
| }, | ||
| { | ||
| "name": "Paper Plane" | ||
| } | ||
| ] | ||
| }, | ||
| "mission": { | ||
| "segments": [ | ||
| { | ||
| "type": "taxi", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Battery #1", | ||
| "time": 120.0, | ||
| "altitude": 0.0 | ||
| }, | ||
| { | ||
| "type": "vertical_climb", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Battery #1", | ||
| "velocity": 8.0, | ||
| "altitude": [0.0, 500.0] | ||
| }, | ||
| { | ||
| "type": "transition", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Battery #1", | ||
| "altitude": 500.0, | ||
| "transition_angle": 40.0, | ||
| "time": 120.0, | ||
| "velocity": [0.0, 40.0] | ||
| }, | ||
| { | ||
| "type": "climb", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Fuel Tank #1", | ||
| "velocity": 40.0, | ||
| "altitude": [500.0, 2500.0], | ||
| "angle": 5 | ||
| }, | ||
| { | ||
| "type": "cruise", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Fuel Tank #1", | ||
| "velocity": 50.0, | ||
| "range": 80000.0, | ||
| "altitude": 2500.0 | ||
| }, | ||
| { | ||
| "type": "descent", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Fuel Tank #1", | ||
| "velocity": -40.0, | ||
| "altitude": [2500.0, 1000.0], | ||
| "angle": -5.0 | ||
| }, | ||
| { | ||
| "type": "hold", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Fuel Tank #1", | ||
| "velocity": 40.0, | ||
| "time": 300.0, | ||
| "altitude": 1000.0 | ||
| }, | ||
| { | ||
| "type": "descent", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Fuel Tank #1", | ||
| "velocity": -40.0, | ||
| "altitude": [1000.0, 400.0], | ||
| "angle": -5.0 | ||
| }, | ||
| { | ||
| "type": "vertical_descent", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Battery #1", | ||
| "velocity": -6.0, | ||
| "altitude": [400.0, 0.0] | ||
| }, | ||
| { | ||
| "type": "landing", | ||
| "propulsion_type": "Prop Engine #1", | ||
| "energy_source": "Battery #1", | ||
| "time": 120.0, | ||
| "altitude": 0.0 | ||
| } | ||
| ] | ||
| }, | ||
| "aircraft": { | ||
| "payload": { | ||
| "mass": 680.0 | ||
| }, | ||
| "structure": { | ||
| "mass": 2000.0 | ||
| }, | ||
| "subsystems": { | ||
| "mass": 50.0 | ||
| }, | ||
| "propulsion_types": [ | ||
| { | ||
| "name": "Prop Engine #1", | ||
| "type": "prop", | ||
| "mass": 500.0, | ||
| "tip_velocity": 240.1, | ||
| "efficiency": 0.5, | ||
| "specific_fuel_consumption": 4.25e-5, | ||
| "ss": 0.08, | ||
| "cd": 0.02, | ||
| "k_i": 1.15, | ||
| "fm": 0.6 | ||
| } | ||
| ], | ||
| "energy_sources": [ | ||
| { | ||
| "name": "Battery #1", | ||
| "type": "electric", | ||
| "specific_energy": 360000.0, | ||
| "efficiency": 0.9, | ||
| "reserve": 0.2 | ||
| }, | ||
| { | ||
| "name": "Fuel Tank #1", | ||
| "type": "fuel", | ||
| "specific_energy": 0.123, | ||
| "reserve": 0.06 | ||
| } | ||
| ], | ||
| "performance": { | ||
| "cd_0": 0.02, | ||
| "aspect_ratio": 5.0, | ||
| "ld_max": 8.0, | ||
| "disc_loading": 900 | ||
| }, | ||
| "components": [ | ||
| { | ||
| "name": "Fuselage", | ||
| "type": "fuselage", | ||
| "interf_factor": 1.0, | ||
| "diameter": 1.0, | ||
| "length": 4.0, | ||
| "area_ref": 1.0, | ||
| "area_wet": 2.0 | ||
| }, | ||
| { | ||
| "name": "Main Wing", | ||
| "type": "wing", | ||
| "interf_factor": 1.0, | ||
| "aspect_ratio": 5.0, | ||
| "span": 10.0, | ||
| "mean_chord": 1.5, | ||
| "airfoil": { | ||
| "type": "naca0012", | ||
| "tc_max": 0.15, | ||
| "xc_max": 0.3, | ||
| "cl_aa": 6.2, | ||
| "cl_max": 2.0 | ||
| }, | ||
| "sweep_le": 10.0, | ||
| "sweep_c4": 15.0, | ||
| "sweep_tc_max": 20.0, | ||
| "area_ref": 15.0, | ||
| "area_wet": 30.0 | ||
| }, | ||
| { | ||
| "name": "Horizontal Tail", | ||
| "type": "wing", | ||
| "interf_factor": 1.0, | ||
| "aspect_ratio": 5.0, | ||
| "span": 2.0, | ||
| "mean_chord": 0.5, | ||
| "airfoil": { | ||
| "type": "naca0012", | ||
| "tc_max": 0.15, | ||
| "xc_max": 0.3, | ||
| "cl_aa": 6.2, | ||
| "cl_max": 2.0 | ||
| }, | ||
| "sweep_le": 10.0, | ||
| "sweep_c4": 15.0, | ||
| "sweep_tc_max": 20.0, | ||
| "area_ref": 1.0, | ||
| "area_wet": 2.0 | ||
| }, | ||
| { | ||
| "name": "Vertical Tail", | ||
| "type": "wing", | ||
| "interf_factor": 1.0, | ||
| "aspect_ratio": 5.0, | ||
| "span": 2.0, | ||
| "mean_chord": 1.0, | ||
| "airfoil": { | ||
| "type": "naca0012", | ||
| "tc_max": 0.15, | ||
| "xc_max": 0.3, | ||
| "cl_aa": 6.2, | ||
| "cl_max": 2.0 | ||
| }, | ||
| "sweep_le": 10.0, | ||
| "sweep_c4": 15.0, | ||
| "sweep_tc_max": 20.0, | ||
| "area_ref": 2.0, | ||
| "area_wet": 4.0 | ||
| } | ||
| ] | ||
| } | ||
| } |