Class: `NitrousOxide`

Description

The NitrousOxide class represents the properties and constants for Nitrous Oxide (N₂O).
It provides physical and thermodynamic properties required in process engineering simulations and calculations.
All constants are from Perry's Chemical Engineers' Handbook, 8th ed., Section 2 (compound no. 252).

Properties

name (string): Nitrous Oxide
formula (string): N₂O
molecular_weight (float): 44.013 g/mol

Class Reference

class NitrousOxide()

Parameters:
* temperature: Temperature, default = Temperature(25,"C")
* pressure: Pressure, default = Pressure(1,"atm")
* density: Density, default = None
* specific_heat: SpecificHeat, default = None
* viscosity: Viscosity, default = None
* thermal_conductivity: ThermalConductivity, default = None
* vapor_pressure: Pressure, default = None
* enthalpy: HeatOfVaporization, default = None
* phase: str, default = None ("liquid" or "gas" overrides the vapor-pressure test)

Methods

The properties of the NitrousOxide class are calculated using the following methods, inherited from the base Component class.

phase(): Detects the phase of the substance ("liquid" or "gas") by comparing the system pressure and vapor pressure. (At standard conditions nitrous oxide is a gas; it boils at 184.7 K (-88.4 °C) at 1 atm by its Table 2-8 row.)
density():
Liquid Phase: DIPPR Eq. 105 (Perry's Table 2-32)
Gas Phase: Uses the Ideal Gas Law
specific_heat():
Liquid Phase: Polynomial function of temperature (Perry's Table 2-153)
Gas Phase: Ideal-gas heat capacity (Cp), DIPPR Eq. 107 (Perry's Table 2-156)
viscosity():
Liquid Phase: DIPPR Eq. 101 (Perry's Table 2-313)
Gas Phase: Uses Sutherland’s Law with the base class's air constants (no gas viscosity data for this component yet)
thermal_conductivity():
Liquid Phase: Polynomial function of temperature (Perry's Table 2-315)
Gas Phase: Vapor thermal conductivity (k), DIPPR Eq. 102 (Perry's Table 2-314)
vapor_pressure(): DIPPR Eq. 101 (Perry's Table 2-8).
enthalpy(): Enthalpy of vaporization (ΔHvap), DIPPR Eq. 106 (Perry's Table 2-150). It is 0 above the critical temperature.

Examples

from processpi.components import NitrousOxide
from processpi.units import *

n2o = NitrousOxide(temperature=Temperature(25, "C"))
print(n2o.phase())
print(n2o.density().to("kg/m3"))
print(n2o.viscosity().to("Pa·s"))
print(n2o.specific_heat().to("J/kgK"))
print(n2o.thermal_conductivity().to("W/mK"))
print(n2o.vapor_pressure().to("Pa"))
print(n2o.enthalpy().to("J/kg"))

Output

gas
1.798989 kg/m3
1.8e-05 Pa·s (dynamic)
878.540809 J/kgK
0.017433 W/mK
5729121.826386 Pa
148552.544509 J/kg

Class: NitrousOxide