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

generate_int_stations(NSD, ETA)

Divides half of the wing in integration stations

Assumptions:

Source:

The Flight Optimization System Weight Estimation Method

Inputs:

NSD: number of integration stations requested ETA: list of spanwise locations of all sections of the wing

Outputs:

NS: actual number of integration stations Y: spanwise locations of the integrations stations normalized by half span

Properties Used:

N/A