AircraftBasicDescentModel#
- class ansys.stk.core.stkobjects.aviator.AircraftBasicDescentModel#
Bases:
IPerformanceModel
,ICatalogItem
Class defining the basic descent performance model for an Aviator aircraft.
Overview#
Set the airspeed type and value. |
|
Get the catalog item interface for this object. |
Get or set the ceiling altitude. |
|
Get the airsepeed. |
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Get the airspeed type. |
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Get or set the altitude rate. |
|
Get or set whether to use Aero/Propulsion fuel flow. |
|
Get or set whether to scale fuel flow by non std density. |
|
Get or set the Sea Level Fuel Flow. |
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Get or set whether to enable relative airspeed tolerance. |
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Get or set the relative airspeed tolerance. |
Import detail#
from ansys.stk.core.stkobjects.aviator import AircraftBasicDescentModel
Property detail#
- property AircraftBasicDescentModel.airspeed_type: AirspeedType#
Get the airspeed type.
- property AircraftBasicDescentModel.use_aerodynamic_propulsion_fuel: bool#
Get or set whether to use Aero/Propulsion fuel flow.
- property AircraftBasicDescentModel.scale_fuel_flow_by_non_std_density: bool#
Get or set whether to scale fuel flow by non std density.
Method detail#
- AircraftBasicDescentModel.set_airspeed(self, airspeed_type: AirspeedType, airspeed: float) None #
Set the airspeed type and value.
- AircraftBasicDescentModel.get_as_catalog_item(self) ICatalogItem #
Get the catalog item interface for this object.
- Returns:
ICatalogItem