WOLFRAM SYSTEM MODELER
PropulsionBaseInterface for propulsion models |
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Wolfram Language
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SystemModel["Aircraft.Physical.FixedWing.Parts.Propulsions.Interfaces.PropulsionBase"]
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Information
This class is the propulsion system base model, which the ConventionalPropulsion and CustomPropulsion models extend.
In this class, the parameters and variables that are used in all propulsion system models and are required by the AircraftBase model are declared. Additionally, the frame connected to the aircraft reference point is declared in this class.
Parameters (11)
| kSkinNac |
Type: Length (m) Description: Nacelle surface roughness height |
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| CADshapes |
Type: Boolean Description: true, if external CAD files are used for animation |
| convProp |
Type: Boolean Description: =true, if conventional propulsion |
| weightEst |
Type: Boolean Description: true, if weight estimation method is used for masses, center of mass location and inertia tensor |
| SrefWing |
Type: Area (m²) Description: Main wing reference area |
| nEng |
Type: Integer Description: Number of engines |
| T0 |
Type: Temperature (K) Description: Temperature at sea-level |
| rho0 |
Type: Density (kg/m³) Description: Air density at sea-level |
| p0 |
Type: Pressure (Pa) Description: Static pressure at sea-level |
| gammaAir |
Type: Real Description: Adiabatic index for air |
| bWing |
Type: Length (m) Description: Main wing span |
Inputs (1)
| flightData |
Type: FlightData Description: Global flight data variables |
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Connectors (1)
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aircraftRP |
Type: Frame_b Description: Connector to aircraft reference point |
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Components (1)
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flightData |
Type: FlightData Description: Global flight data variables |
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Extended by (2)
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Aircraft.Physical.FixedWing.Parts.Propulsions.Interfaces Interface for custom propulsion model |
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Aircraft.Physical.FixedWing.Parts.Propulsions.Interfaces Interface for conventional propulsion model |