RCAIDE.Library.Methods.Powertrain.Propulsors.Turbojet

Turbojet

Contains methods for analyzing and designing turbojet propulsion systems. This module provides functionality for computing thrust, sizing engine cores, and evaluating turbojet performance characteristics.

See also

RCAIDE.Library.Components.Powertrain.Converters.Ram, RCAIDE.Library.Components.Powertrain.Converters.Combustor, RCAIDE.Library.Components.Powertrain.Converters.Compressor, RCAIDE.Library.Components.Powertrain.Converters.Turbine, RCAIDE.Library.Components.Powertrain.Converters.Expansion_Nozzle

Modules

append_turbojet_conditions(propulsor, ...)	Initializes turbojet operating conditions for a mission segment.
compute_thurst
compute_turbojet_performance(turbojet, state)	Computes the performance of a turbojet engine by analyzing the thermodynamic cycle.
design_turbojet(turbojet)	Designs a turbojet engine by computing performance properties and sizing components based on design conditions.
size_core(turbojet, conditions)	Sizes the core flow for a turbojet engine at the design condition.