RCAIDE.Library.Methods.Geometry.Planform.fuselage_planform
fuselage_planform#
- fuselage_planform(fuselage, circular_cross_section=True)[source]#
Calculates fuselage geometry values
Assumptions: None
Source: http://adg.stanford.edu/aa241/drag/wettedarea.html
Inputs: fuselage.
num_coach_seats [-] fineness.nose [-] fineness.tail [-] width [m] heights.maximum [m]
Outputs: fuselage.
lengths.nose [m] lengths.tail [m] lengths.cabin [m] lengths.total [m] areas.wetted [m] areas.front_projected [m] effective_diameter [m]
Properties Used: N/A