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

FLOPS

Methods for computing component weights specific to Blended Wing Body (BWB) aircraft configurations. This module provides specialized weight estimation techniques that account for the unique structural and geometric characteristics of BWB designs.

See also

RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Common

Shared component weight methods

RCAIDE.Library.Methods.Mass_Properties.Weight_Buildups.Conventional.Transport

Transport aircraft weight methods

Modules

compute_aft_centerbody_weight(no_of_engines, ...)	Computes the structural weight of the aft section of a BWB centerbody using regression-based methods.
compute_cabin_weight(cabin_area, TOGW)	Computes the structural weight of the pressurized cabin section of a BWB aircraft using regression-based methods derived from FEA studies.
compute_operating_empty_weight(vehicle[, ...])	This is for a BWB aircraft configuration.