Source code for armi.materials.tZM

# Copyright 2019 TerraPower, LLC
#
# Licensed under the Apache License, Version 2.0 (the "License");
# you may not use this file except in compliance with the License.
# You may obtain a copy of the License at
#
#     http://www.apache.org/licenses/LICENSE-2.0
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# Unless required by applicable law or agreed to in writing, software
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"""
TZM
"""
from numpy import interp

from armi.materials.material import Material
from armi.utils.units import getTc


[docs]class TZM(Material): name = "TZM" references = { "linear expansion percent": "Report on the Mechanical and Thermal Properties of Tungsten and TZM Sheet Produced \ in the Refractory Metal Sheet Rolling Program, Part 1 to Bureau of Naval Weapons Contract No. N600(19)-59530, \ Southern Research Institute" } temperatureC = [ 21.11, 456.11, 574.44, 702.22, 840.56, 846.11, 948.89, 1023.89, 1146.11, 1287.78, 1382.22, ] percentThermalExpansion = [ 0, 1.60e-01, 2.03e-01, 2.53e-01, 3.03e-01, 3.03e-01, 3.42e-01, 3.66e-01, 4.21e-01, 4.68e-01, 5.04e-01, ]
[docs] def setDefaultMassFracs(self): self.setMassFrac("C", 2.50749e-05) self.setMassFrac("TI", 0.002502504) self.setMassFrac("ZR", 0.000761199) self.setMassFrac("MO", 0.996711222)
[docs] def density(self, Tk=None, Tc=None): return 10.16 # g/cc
[docs] def linearExpansionPercent(self, Tk=None, Tc=None): r""" return linear expansion in %dL/L from interpolation of tabular data. This function is used to expand a material from its reference temperature (21C) to a particular hot temperature. Parameters ---------- Tk : float temperature in K Tc : float temperature in C Source: Report on the Mechanical and Thermal Properties of Tungsten and TZM Sheet Produced \ in the Refractory Metal Sheet Rolling Program, Part 1 to Bureau of Naval Weapons Contract No. N600(19)-59530, 1966 \ Southern Research Institute. See Table viii-b, Appendix B, page 181. """ Tc = getTc(Tc, Tk) self.checkTempRange(21.11, 1382.22, Tc, "linear expansion percent") return interp(Tc, self.temperatureC, self.percentThermalExpansion)