TY - JOUR
T1 - New isothermal vapor-liquid equilibria for the CO2 + n-nonane, and CO2 + n-undecane systems
AU - Camacho-Camacho, Luis E.
AU - Galicia-Luna, Luis A.
AU - Elizalde-Solis, Octavio
AU - Martínez-Ramírez, Zenaido
N1 - Funding Information:
The authors thank to Conacyt and IPN for the financial support.
PY - 2007/10/1
Y1 - 2007/10/1
N2 - Experimental vapor-liquid equilibria (VLE) for the CO2 + n-nonane and CO2 + n-undecane systems were obtained by using a 100-cm3 high-pressure titanium cell up to 20 MPa at four temperatures (315, 344, 373, and 418 K). The apparatus is based on the static-analytic method; which allows fast determination of the coexistence curve. For the CO2 + n-nonane system, good agreement was found between the experimental data and those reported in literature. No literature data were available for the CO2 + n-undecane system at high temperature and pressure. Experimental data were correlated with the Peng-Robinson equation of state using the classical and the Wong-Sandler mixing rules.
AB - Experimental vapor-liquid equilibria (VLE) for the CO2 + n-nonane and CO2 + n-undecane systems were obtained by using a 100-cm3 high-pressure titanium cell up to 20 MPa at four temperatures (315, 344, 373, and 418 K). The apparatus is based on the static-analytic method; which allows fast determination of the coexistence curve. For the CO2 + n-nonane system, good agreement was found between the experimental data and those reported in literature. No literature data were available for the CO2 + n-undecane system at high temperature and pressure. Experimental data were correlated with the Peng-Robinson equation of state using the classical and the Wong-Sandler mixing rules.
KW - Equation of state
KW - Static-analytic method
KW - Vapor-liquid equilibria
UR - http://www.scopus.com/inward/record.url?scp=34547655634&partnerID=8YFLogxK
U2 - 10.1016/j.fluid.2007.04.022
DO - 10.1016/j.fluid.2007.04.022
M3 - Artículo
SN - 0378-3812
VL - 259
SP - 45
EP - 50
JO - Fluid Phase Equilibria
JF - Fluid Phase Equilibria
IS - 1 SPEC. ISS.
ER -