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

FLOPS

RCAIDE Package Setup

Modules

compute_fuselage_weight(vehicle)	Calculate the weight of a general aviation aircraft fuselage using NASA FLOPS methodology.
compute_horizontal_tail_weight(vehicle)	Calculates the weight of an aircraft's horizontal tail using FLOPS methodology.
compute_landing_gear_weight(vehicle)	Calculates the weight of a general aviation aircraft's landing gear system using FLOPS methodology.
compute_operating_empty_weight(vehicle[, ...])	"Computes the operating empty weight of a vehicle
compute_operating_items_weight(vehicle)	Calculate the weight of aircraft operating items using FLOPS methodology for a general aviation aircraft.
compute_propulsion_system_weight(vehicle, ...)	Calculate the weight of the complete propulsion system using FLOPS methodology.
compute_systems_weight(vehicle)	Calculate the systems weight for general aviation aircraft using FLOPS methodology.
compute_vertical_tail_weight(vehicle, wing)	Calculate the vertical tail weight for general aviation aircraft using FLOPS methodology.
compute_wing_weight(vehicle, wing, WPOD, ...)	Calculate the wing weight using FLOPS methodology for general aviation aircraft. The wing weight consists of: