RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_bwb_wing_weight.get_spanwise_engine

get_spanwise_engine(networks, SEMISPAN)

Returns EETA for the engine locations along the wing

Assumptions:

Source:

The Flight Optimization System Weight Estimation Method

Inputs:

networks: data dictionary with all the engine properties

-.wing_mounted: list of boolean if engine is mounted to wing -.number_of_engines: number of engines -.origin: origin of the engine

SEMISPAN: half span [m]

Outputs:

EETA: span wise locations of the engines mounted to the wing normalized by the half span

Properties Used:

N/A