RCAIDE.Library.Methods.Powertrain.Converters.Supersonic_Nozzle.append_supersonic_nozzle_conditions
append_supersonic_nozzle_conditions#
- append_supersonic_nozzle_conditions(supersonic_nozzle, segment, energy_conditions)[source]#
Initializes and appends supersonic nozzle conditions data structures to the propulsor conditions dictionary.
- Parameters:
supersonic_nozzle (SupersonicNozzle) – The supersonic nozzle component for which conditions are being initialized.
segment (Segment) – The mission segment in which the supersonic nozzle is operating.
energy_conditions (dict) – Dictionary containing conditions for all propulsion components.
- Returns:
This function modifies the propulsor_conditions dictionary in-place.
- Return type:
None
Notes
This function creates empty Conditions objects for the supersonic nozzle’s inputs and outputs within the propulsor_conditions dictionary. These conditions will be populated during the mission analysis process.