Source code for RCAIDE.Library.Methods.Powertrain.Converters.Compressor.append_compressor_conditions
# RCAIDE/Library/Methods/Powertrain/Converters/compressor/append_compressor_conditions.py
# (c) Copyright 2023 Aerospace Research Community LLC
#
# Created: Jun 2024, M. Clarke
from RCAIDE.Framework.Mission.Common import Conditions
# ----------------------------------------------------------------------------------------------------------------------
# append_compressor_conditions
# ----------------------------------------------------------------------------------------------------------------------
[docs]
def append_compressor_conditions(compressor,segment,energy_conditions):
"""
Initializes empty condition containers for compressor analysis in the propulsion system.
Parameters
----------
compressor : Compressor
The compressor component being analyzed
segment : Segment
The mission segment being analyzed
energy_conditions : Conditions
Container for storing energy system conditions
Returns
-------
None
Notes
-----
This function creates empty Conditions containers that will be populated
during compressor performance calculations with thermodynamic states
and operating parameters.
See Also
--------
RCAIDE.Library.Methods.Powertrain.Converters.Compressor.compute_compressor_performance
"""
ones_row = segment.state.ones_row
energy_conditions.converters[compressor.tag] = Conditions()
energy_conditions.converters[compressor.tag].inputs = Conditions()
energy_conditions.converters[compressor.tag].outputs = Conditions()
energy_conditions.converters[compressor.tag].outputs.external_shaft_work_done = 0*ones_row(1)
energy_conditions.converters[compressor.tag].outputs.external_electrical_power = 0*ones_row(1)
return
