RCAIDE.Library.Methods.Geometry.Planform.wing_fuel_volume wing_fuel_volume# wing_fuel_volume(wing)[source]# Calculates the available fuel volume in a wing. Assumptions: None Source: Torenbeek, E., “Advanced Aircraft Design”, 2013 (equation 10.30) Inputs: wing. areas.reference [m^2] aspect_ratio [-] thickness_to_chord [-] Outputs: wing.volume [m^3] Properties Used: N/A