RCAIDE.Library.Methods.Aerodynamics.Common.Drag.parasite_total
parasite_total#
- parasite_total(state, settings, geometry)[source]#
Sums up the parasite drags from all compoments
- Assumptions:
None
- Source:
None
- Parameters:
state (dict) – flight conditions [-]
settings (dict) – analyses settings [-]
geometry (dict) – aircraft data stucture [-]
conditions.aerodynamics.coefficients.drag. – parasite[wing.tag(s)].parasite_drag (numpy.ndarray): wing parasite drags [Unitless] parasite[fuselage.tag(s)].parasite_drag (numpy.ndarray): fuselage parasite drags [Unitless] parasite[boom.tag(s)].parasite_drag (numpy.ndarray): boom parasite drags [Unitless] parasite[nacelle.tag(s)].parasite_drag (numpy.ndarray): nacelle parasite drags [Unitless] parasite[pylon.tag(s)].parasite_drag (numpy.ndarray): pylon parasite drags [Unitless]
- Returns:
None