RCAIDE.Library.Methods.Aerodynamics.Common.Drag.asymmetry_drag
asymmetry_drag#
- asymmetry_drag(state, geometry, engine_out_location=0, single_engine_thrust=0, windmilling_drag_coefficient=0.0)[source]#
Computes asymmetry drag due to engine failure
Assumptions: Two engine aircraft
Source: Unknown source
Inputs: state.conditions.freestream.dynamic_pressure [Pa] state.conditions.aerodynamics.drag_breakdown.windmilling_drag.windmilling_drag_coefficient [Unitless] geometry.
mass_properties.center_of_gravity [m] networks.
number_of_engines [Unitless]
- wings.
tag sref (this function probably doesn’t run) [m^2] spans.projected [m]
reference_area [m^2]
Outputs: asymm_trim_drag_coefficient [Unitless] (packed in state.conditions.aerodynamics.drag_breakdown.asymmetry_trim_coefficient)
Properties Used: N/A