Isobaric Properties for Oxygen
- Fluid Data
- Auxiliary Data
- References and Notes
- Notes
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Fluid Data
Isobaric Data for P = 0.020000 MPa
Temperature (K) | Pressure (MPa) | Density (kg/m3) | Volume (m3/kg) | Internal Energy (kJ/mol) | Enthalpy (kJ/mol) | Entropy (J/mol*K) | Cv (J/mol*K) | Cp (J/mol*K) | Sound Spd. (m/s) | Joule-Thomson (K/MPa) | Viscosity (uPa*s) | Therm. Cond. (W/m*K) | Phase |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
54.361 | 0.020000 | 1306.1 | 0.00076564 | -6.1955 | -6.1950 | 66.944 | 38.250 | 53.538 | 1123.4 | -0.37994 | 773.75 | 0.20194 | liquid |
59.361 | 0.020000 | 1284.8 | 0.00077831 | -5.9281 | -5.9276 | 71.650 | 35.075 | 53.524 | 1129.4 | -0.37115 | 596.71 | 0.19487 | liquid |
64.361 | 0.020000 | 1262.6 | 0.00079202 | -5.6602 | -5.6596 | 75.985 | 33.610 | 53.658 | 1105.8 | -0.36395 | 471.19 | 0.18776 | liquid |
69.361 | 0.020000 | 1239.9 | 0.00080652 | -5.3918 | -5.3912 | 80.001 | 32.642 | 53.695 | 1071.2 | -0.35770 | 381.37 | 0.18065 | liquid |
74.361 | 0.020000 | 1216.9 | 0.00082178 | -5.1233 | -5.1227 | 83.739 | 31.841 | 53.713 | 1032.6 | -0.35073 | 315.75 | 0.17353 | liquid |
77.100 | 0.020000 | 1204.1 | 0.00083049 | -4.9761 | -4.9756 | 85.682 | 31.438 | 53.745 | 1010.7 | -0.34617 | 287.15 | 0.16963 | liquid |
77.100 | 0.020000 | 1.0081 | 0.99194 | 1.5812 | 2.2160 | 178.96 | 22.417 | 31.282 | 165.48 | 44.024 | 5.9195 | 0.0067231 | vapor |
79.361 | 0.020000 | 0.97838 | 1.0221 | 1.6311 | 2.2852 | 179.84 | 21.433 | 30.095 | 168.63 | 32.571 | 6.0989 | 0.0069464 | vapor |
84.361 | 0.020000 | 0.91907 | 1.0881 | 1.7369 | 2.4332 | 181.65 | 20.804 | 29.321 | 174.48 | 23.269 | 6.4930 | 0.0074395 | vapor |
89.361 | 0.020000 | 0.86675 | 1.1537 | 1.8411 | 2.5795 | 183.34 | 20.746 | 29.228 | 179.73 | 20.702 | 6.8839 | 0.0079310 | vapor |
94.361 | 0.020000 | 0.82014 | 1.2193 | 1.9453 | 2.7256 | 184.93 | 20.773 | 29.237 | 184.76 | 19.321 | 7.2714 | 0.0084208 | vapor |
99.361 | 0.020000 | 0.77832 | 1.2848 | 2.0496 | 2.8718 | 186.44 | 20.799 | 29.249 | 189.65 | 18.087 | 7.6555 | 0.0089084 | vapor |
104.36 | 0.020000 | 0.74059 | 1.3503 | 2.1540 | 3.0181 | 187.87 | 20.815 | 29.251 | 194.41 | 16.871 | 8.0362 | 0.0093939 | vapor |
109.36 | 0.020000 | 0.70637 | 1.4157 | 2.2583 | 3.1643 | 189.24 | 20.822 | 29.245 | 199.06 | 15.695 | 8.4135 | 0.0098770 | vapor |
114.36 | 0.020000 | 0.67520 | 1.4810 | 2.3627 | 3.3105 | 190.55 | 20.825 | 29.236 | 203.60 | 14.589 | 8.7874 | 0.010358 | vapor |
119.36 | 0.020000 | 0.64668 | 1.5464 | 2.4671 | 3.4567 | 191.80 | 20.825 | 29.226 | 208.04 | 13.569 | 9.1579 | 0.010836 | vapor |
124.36 | 0.020000 | 0.62049 | 1.6116 | 2.5714 | 3.6028 | 193.00 | 20.824 | 29.216 | 212.39 | 12.637 | 9.5250 | 0.011311 | vapor |
129.36 | 0.020000 | 0.59635 | 1.6769 | 2.6757 | 3.7489 | 194.15 | 20.822 | 29.206 | 216.65 | 11.793 | 9.8889 | 0.011784 | vapor |
134.36 | 0.020000 | 0.57402 | 1.7421 | 2.7800 | 3.8949 | 195.26 | 20.819 | 29.197 | 220.83 | 11.030 | 10.249 | 0.012254 | vapor |
139.36 | 0.020000 | 0.55331 | 1.8073 | 2.8842 | 4.0408 | 196.33 | 20.817 | 29.188 | 224.92 | 10.340 | 10.607 | 0.012722 | vapor |
144.36 | 0.020000 | 0.53406 | 1.8725 | 2.9884 | 4.1868 | 197.35 | 20.815 | 29.181 | 228.95 | 9.7165 | 10.961 | 0.013187 | vapor |
149.36 | 0.020000 | 0.51610 | 1.9376 | 3.0926 | 4.3326 | 198.35 | 20.813 | 29.175 | 232.90 | 9.1510 | 11.312 | 0.013649 | vapor |
154.36 | 0.020000 | 0.49931 | 2.0027 | 3.1968 | 4.4785 | 199.31 | 20.812 | 29.170 | 236.78 | 8.6371 | 11.659 | 0.014109 | vapor |
159.36 | 0.020000 | 0.48359 | 2.0679 | 3.3010 | 4.6243 | 200.24 | 20.811 | 29.165 | 240.60 | 8.1689 | 12.004 | 0.014566 | vapor |
164.36 | 0.020000 | 0.46883 | 2.1330 | 3.4051 | 4.7702 | 201.14 | 20.810 | 29.161 | 244.36 | 7.7409 | 12.346 | 0.015020 | vapor |
169.36 | 0.020000 | 0.45494 | 2.1981 | 3.5092 | 4.9160 | 202.01 | 20.810 | 29.158 | 248.06 | 7.3485 | 12.685 | 0.015472 | vapor |
174.36 | 0.020000 | 0.44186 | 2.2632 | 3.6134 | 5.0617 | 202.86 | 20.810 | 29.156 | 251.71 | 6.9877 | 13.020 | 0.015921 | vapor |
179.36 | 0.020000 | 0.42951 | 2.3282 | 3.7175 | 5.2075 | 203.69 | 20.810 | 29.154 | 255.30 | 6.6548 | 13.353 | 0.016367 | vapor |
184.36 | 0.020000 | 0.41783 | 2.3933 | 3.8216 | 5.3533 | 204.49 | 20.811 | 29.153 | 258.84 | 6.3468 | 13.683 | 0.016811 | vapor |
189.36 | 0.020000 | 0.40678 | 2.4584 | 3.9257 | 5.4990 | 205.27 | 20.813 | 29.153 | 262.34 | 6.0611 | 14.011 | 0.017253 | vapor |
194.36 | 0.020000 | 0.39629 | 2.5234 | 4.0299 | 5.6448 | 206.03 | 20.815 | 29.153 | 265.78 | 5.7953 | 14.335 | 0.017692 | vapor |
199.36 | 0.020000 | 0.38633 | 2.5885 | 4.1340 | 5.7906 | 206.77 | 20.817 | 29.154 | 269.18 | 5.5473 | 14.657 | 0.018128 | vapor |
204.36 | 0.020000 | 0.37686 | 2.6535 | 4.2382 | 5.9363 | 207.49 | 20.821 | 29.156 | 272.53 | 5.3155 | 14.977 | 0.018562 | vapor |
209.36 | 0.020000 | 0.36784 | 2.7185 | 4.3423 | 6.0821 | 208.19 | 20.824 | 29.159 | 275.85 | 5.0983 | 15.293 | 0.018994 | vapor |
214.36 | 0.020000 | 0.35925 | 2.7836 | 4.4465 | 6.2279 | 208.88 | 20.829 | 29.162 | 279.12 | 4.8943 | 15.607 | 0.019424 | vapor |
219.36 | 0.020000 | 0.35105 | 2.8486 | 4.5507 | 6.3738 | 209.55 | 20.835 | 29.167 | 282.35 | 4.7023 | 15.919 | 0.019851 | vapor |
224.36 | 0.020000 | 0.34321 | 2.9136 | 4.6549 | 6.5196 | 210.21 | 20.841 | 29.172 | 285.54 | 4.5213 | 16.228 | 0.020276 | vapor |
229.36 | 0.020000 | 0.33572 | 2.9787 | 4.7592 | 6.6655 | 210.86 | 20.848 | 29.179 | 288.70 | 4.3503 | 16.535 | 0.020698 | vapor |
234.36 | 0.020000 | 0.32855 | 3.0437 | 4.8635 | 6.8114 | 211.48 | 20.857 | 29.186 | 291.81 | 4.1885 | 16.839 | 0.021119 | vapor |
239.36 | 0.020000 | 0.32168 | 3.1087 | 4.9679 | 6.9573 | 212.10 | 20.866 | 29.194 | 294.89 | 4.0352 | 17.141 | 0.021537 | vapor |
244.36 | 0.020000 | 0.31509 | 3.1737 | 5.0722 | 7.1033 | 212.70 | 20.876 | 29.204 | 297.94 | 3.8897 | 17.441 | 0.021953 | vapor |
249.36 | 0.020000 | 0.30876 | 3.2387 | 5.1767 | 7.2494 | 213.30 | 20.888 | 29.215 | 300.95 | 3.7513 | 17.739 | 0.022367 | vapor |
254.36 | 0.020000 | 0.30269 | 3.3037 | 5.2812 | 7.3955 | 213.88 | 20.900 | 29.227 | 303.93 | 3.6196 | 18.034 | 0.022779 | vapor |
259.36 | 0.020000 | 0.29685 | 3.3687 | 5.3857 | 7.5417 | 214.45 | 20.914 | 29.240 | 306.88 | 3.4941 | 18.327 | 0.023189 | vapor |
264.36 | 0.020000 | 0.29123 | 3.4337 | 5.4904 | 7.6879 | 215.00 | 20.929 | 29.254 | 309.79 | 3.3743 | 18.619 | 0.023597 | vapor |
269.36 | 0.020000 | 0.28582 | 3.4987 | 5.5951 | 7.8342 | 215.55 | 20.945 | 29.270 | 312.68 | 3.2599 | 18.908 | 0.024003 | vapor |
274.36 | 0.020000 | 0.28060 | 3.5637 | 5.6999 | 7.9806 | 216.09 | 20.963 | 29.287 | 315.53 | 3.1505 | 19.194 | 0.024407 | vapor |
279.36 | 0.020000 | 0.27558 | 3.6287 | 5.8048 | 8.1271 | 216.62 | 20.981 | 29.305 | 318.36 | 3.0458 | 19.479 | 0.024809 | vapor |
284.36 | 0.020000 | 0.27073 | 3.6937 | 5.9098 | 8.2736 | 217.14 | 21.001 | 29.325 | 321.15 | 2.9454 | 19.762 | 0.025209 | vapor |
289.36 | 0.020000 | 0.26605 | 3.7587 | 6.0148 | 8.4203 | 217.65 | 21.023 | 29.346 | 323.92 | 2.8492 | 20.043 | 0.025608 | vapor |
Auxiliary Data
Reference States
Enthalpy | unknown |
---|---|
Entropy | unknown |
Additional fluid properties
Critical temperature (Tc) | 154.581 K |
---|---|
Critical pressure (Pc) | 5.0430 MPa |
Critical density (Dc) | 436.1 kg/m3 |
Acentric factor | 0.0222 |
Normal boiling point | 90.1878 K |
Dipole moment | 0.0 Debye |
References and Notes
Equation of state
Schmidt, R.; Wagner, W., A New Form of the Equation of State for Pure Substances and its Application to Oxygen, Fluid Phase Equilib., 1985, 19, 3, 175-200, https://doi.org/10.1016/0378-3812(85)87016-3 . [all data]Schmidt, R. and Wagner, W., "A New Form of the Equation of State for Pure Substances and its Application to Oxygen," Fluid Phase Equilib., 19:175-200, 1985.
also published in:
Stewart, R.B., Jacobsen, R.T, and Wagner, W., "Thermodynamic Properties of Oxygen from the Triple Point to 300 K with Pressures to 80 MPa," J. Phys. Chem. Ref. Data, 20(5):917-1021, 1991.
The uncertainties of the equation of state are 0.15% in vapor pressure, 0.1% in density, 2% in heat capacity, and 1% in the speed of sound, except in the critical region.
Auxillary model, Cp0
Refit by Roland Span of the Schmidt and Wagner equation listed below to account for the electronic contribution up to 2000 K with Planck-Einstein terms only.
Schmidt, R. and Wagner, W., "A New Form of the Equation of State for Pure Substances and its Application to Oxygen," Fluid Phase Equilib., 19:175-200, 1985.
Auxillary model, PX0
Refit by Roland Span of the Schmidt and Wagner equation listed below to account for the electronic contribution up to 2000 K with Planck-Einstein terms only.
Schmidt, R. and Wagner, W., "A New Form of the Equation of State for Pure Substances and its Application to Oxygen," Fluid Phase Equilib., 19:175-200, 1985.
Auxillary model, PH0
Refit by Roland Span of the Schmidt and Wagner equation listed above.
Viscosity
Lemmon, E.W.; Jacobsen, R.T., Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air, Int. J. Thermophys., 2004, 25, 1, 21-69, https://doi.org/10.1023/B:IJOT.0000022327.04529.f3 . [all data]Lemmon, E.W. and Jacobsen, R.T, "Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air," Int. J. Thermophys., 25:21-69, 2004.
The uncertainty is 1% in the dilute gas at temperatures above 200 K, and 5% in the dilute gas at lower temperatures. The uncertainty is around 2% between 270 and 300 K, and increases to 5% outside of this region. The uncertainty may be higher in the liquid near the triple point.
Auxillary model, the collision integral
Lemmon, E.W. and Jacobsen, R.T, 2004.
Thermal conductivity
Lemmon, E.W.; Jacobsen, R.T., Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air, Int. J. Thermophys., 2004, 25, 1, 21-69, https://doi.org/10.1023/B:IJOT.0000022327.04529.f3 . [all data]Lemmon, E.W. and Jacobsen, R.T, "Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air," Int. J. Thermophys., 25:21-69, 2004.
The uncertainty for the dilute gas is 2% with increasing uncertainties near the triple point. The uncertainties range from 3% between 270 and 300 K to 5% elsewhere. The uncertainties above 100 MPa are not known due to a lack of experimental data.
Auxillary model, the thermal conductivity critical enhancement
Lemmon, E.W. and Jacobsen, R.T, 2004.
Surface tension
Mulero, A.; Cachadiña, I.; Parra, M.I., Recommended Correlations for the Surface Tension of Common Fluids, J. Phys. Chem. Ref. Data, 2012, 41, 4, 043105, https://doi.org/10.1063/1.4768782 . [all data]Dielectric constant
Harvey, A.H.; Lemmon, E.W., Method for Estimating the Dielectric Constant of Natural Gas Mixtures, Int. J. Thermophys., 2005, 26, 1, 31-46, https://doi.org/10.1007/s10765-005-2351-5 . [all data]Metling line
Schmidt, R.; Wagner, W., A New Form of the Equation of State for Pure Substances and its Application to Oxygen, Fluid Phase Equilib., 1985, 19, 3, 175-200, https://doi.org/10.1016/0378-3812(85)87016-3 . [all data]Schmidt, R. and Wagner, W., "A New Form of the Equation of State for Pure Substances and its Application to Oxygen," Fluid Phase Equilib., 19:175-200, 1985.
Sublimation line
Lemmon, E.W., 2003.
Vapor pressure
Cullimore, I.D., 2010.
Functional Form: P=Pc*EXP[SUM(Ni*Theta^ti)*Tc/T] where Theta=1-T/Tc, Tc and Pc are the reducing parameters below, which are followed by rows containing Ni and ti.
Saturated liquid density
Cullimore, I.D., 2010.
Functional Form: D=Dc*[1+SUM(Ni*Theta^ti)] where Theta=1-T/Tc, Tc and Dc are the reducing parameters below, which are followed by rows containing Ni and ti.
Saturated liquid volume
Cullimore, I.D., 2010.
Functional Form: D=Dc*EXP[SUM(Ni*Theta^ti)] where Theta=1-T/Tc, Tc and Dc are the reducing parameters below, which are followed by rows containing Ni and ti.
Notes
- Data from NIST Standard Reference Database 69: NIST Chemistry WebBook
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