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