Source code for RCAIDE.Library.Methods.Thermal_Management.Batteries.Air_Cooled.append_air_cooled_conditions
# RCAIDE/Library/Methods/Thermal_Management/Batteries/Air_Cooled/append_air_cooled_conditions.py
#
# Created: Aug 2024, S. Shekar
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# IMPORT
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from RCAIDE.Framework.Mission.Common import Conditions
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# append_turbofan_conditions
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[docs]
def append_air_cooled_conditions(air_cooled,segment,coolant_line):
""" Packs the initial air cooling heat acqusition conditions
Assumptions:
None
Source:
N/A
Inputs:
air_cooled (data structure) [None]
Outputs:
segment
effectiveness [boolean]
total_heat_removed [watts]
Properties Used:
None
"""
ones_row = segment.state.ones_row
segment.state.conditions.energy[coolant_line.tag][air_cooled.tag] = Conditions()
segment.state.conditions.energy[coolant_line.tag][air_cooled.tag].effectiveness = 0. * ones_row(1)
segment.state.conditions.energy[coolant_line.tag][air_cooled.tag].total_heat_removed = 0. * ones_row(1)
segment.state.conditions.energy[coolant_line.tag][air_cooled.tag].power = 0. * ones_row(1)
return
[docs]
def append_air_cooled_segment_conditions(air_cooled, segment,coolant_line, conditions):
"""Sets the initial air cooled heat acquistion conditions at the start of each segment as the last point from the previous segment
Assumptions:
None
Source:
N/A
Inputs:
air_cooled (data structure) [None]
Outputs:
None
Properties Used:
None
"""
air_cooled_conditions = conditions[coolant_line.tag][air_cooled.tag]
if segment.state.initials:
air_cooled_initials = segment.state.initials.conditions.energy[coolant_line.tag][air_cooled.tag]
air_cooled_conditions.effectiveness[:,0] = air_cooled_initials.effectiveness[-1,0]
air_cooled_conditions.total_heat_removed[:,0] = air_cooled_initials.total_heat_removed[-1,0]
return
