RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.BWB.FLOPS.compute_bwb_wing_weight.calculate_load#

calculate_load(ETA)[source]#

Returns load factor assuming elliptical load distribution

Assumptions:

Source:
The Flight Optimization System Weight Estimation Method

Inputs:
ETA: list of spanwise locations of all sections of the wing

Outputs:

PS: load factor at every location in ETA assuming elliptical load distribution