Carbon capture and storage could significantly reduce carbon dioxide (CO2) emissions. One of the major limitations of this technology is the energy penalty for the compression of CO2 to supercritical conditions. To reduce the power requirements, supercritical carbon dioxide compressors must operate near saturation where phase change effects are important. Nonequilibrium condensation can occur at the leading edge of the compressor, causing performance and stability issues. The characterization of the fluid at these conditions is vital to enable advanced compressor designs at enhanced efficiency levels but the analysis is challenging due to the lack of data on metastable fluid properties. In this paper, we assess the behavior and nucleation characteristics of high-pressure subcooled CO2 during the expansion in a de Laval nozzle. The assessment is conducted with numerical calculations and corroborated by experimental measurements. The Wilson line is determined via optical measurements in the range of 41–82 bar. The state of the metastable fluid is characterized through pressure and density measurements, with the latter obtained in a first-of-its-kind laser interferometry setup. The inlet conditions of the nozzle are moved close to the critical point to allow for reduced margins to condensation. The analysis suggests that direct extrapolation using the Span and Wagner equation of state (S–W EOS) model yields results within 2% of the experimental data. The results are applied to define inlet conditions for a supercritical carbon dioxide compressor. Full-scale compressor experiments demonstrate that the reduced inlet temperature can decrease the shaft power input by 16%.
Skip Nav Destination
Article navigation
April 2018
Research-Article
Characterization of Nonequilibrium Condensation of Supercritical Carbon Dioxide in a de Laval Nozzle
Claudio Lettieri,
Claudio Lettieri
Faculty of Aerospace Engineering,
Delft University of Technology,
Delft 2628, The Netherlands
e-mail: c.lettieri-1@tudelft.nl
Delft University of Technology,
Delft 2628, The Netherlands
e-mail: c.lettieri-1@tudelft.nl
Search for other works by this author on:
Derek Paxson,
Derek Paxson
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: dpaxson@mit.edu
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: dpaxson@mit.edu
Search for other works by this author on:
Zoltan Spakovszky,
Zoltan Spakovszky
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: zolti@mit.edu
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: zolti@mit.edu
Search for other works by this author on:
Peter Bryanston-Cross
Peter Bryanston-Cross
School of Engineering,
Warwick University,
Coventry CV4 7AL, UK
e-mail: P.J.Bryanston-Cross@warwick.ac.uk
Warwick University,
Coventry CV4 7AL, UK
e-mail: P.J.Bryanston-Cross@warwick.ac.uk
Search for other works by this author on:
Claudio Lettieri
Faculty of Aerospace Engineering,
Delft University of Technology,
Delft 2628, The Netherlands
e-mail: c.lettieri-1@tudelft.nl
Delft University of Technology,
Delft 2628, The Netherlands
e-mail: c.lettieri-1@tudelft.nl
Derek Paxson
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: dpaxson@mit.edu
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: dpaxson@mit.edu
Zoltan Spakovszky
Department of Aeronautics and Astronautics,
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: zolti@mit.edu
Massachusetts Institute of Technology,
Cambridge, MA 02139
e-mail: zolti@mit.edu
Peter Bryanston-Cross
School of Engineering,
Warwick University,
Coventry CV4 7AL, UK
e-mail: P.J.Bryanston-Cross@warwick.ac.uk
Warwick University,
Coventry CV4 7AL, UK
e-mail: P.J.Bryanston-Cross@warwick.ac.uk
Contributed by the Cycle Innovations Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received July 25, 2017; final manuscript received August 1, 2017; published online November 7, 2017. Editor: David Wisler.
J. Eng. Gas Turbines Power. Apr 2018, 140(4): 041701 (11 pages)
Published Online: November 7, 2017
Article history
Received:
July 25, 2017
Revised:
August 1, 2017
Citation
Lettieri, C., Paxson, D., Spakovszky, Z., and Bryanston-Cross, P. (November 7, 2017). "Characterization of Nonequilibrium Condensation of Supercritical Carbon Dioxide in a de Laval Nozzle." ASME. J. Eng. Gas Turbines Power. April 2018; 140(4): 041701. https://doi.org/10.1115/1.4038082
Download citation file:
Get Email Alerts
Experimental Characterization of Superheated Ammonia Spray from a Single-hole ECN Spray M Injector
J. Eng. Gas Turbines Power
Improving the Predictive Capability of Empirical Heat Transfer Correlations for Hydrogen Internal Combustion Engines
J. Eng. Gas Turbines Power (October 2025)
The Hybrid Pathway to Flexible Power Turbines: Part IV, Automated Construction of Mesh Derived Thermal Network Models for Fast Full-Machine Thermal Analysis
J. Eng. Gas Turbines Power (October 2025)
Related Articles
Modeling Multiphase Effects in CO 2 Compressors at Subcritical Inlet Conditions
J. Eng. Gas Turbines Power (August,2019)
Numerical Investigation of the Flow Behavior Inside a Supercritical CO 2 Centrifugal Compressor
J. Eng. Gas Turbines Power (December,2018)
An Investigation of Real Gas Effects in Supercritical CO 2 Centrifugal Compressors
J. Turbomach (September,2015)
Thermodynamics and Fluid Mechanics of a Closed Blade Cascade Wind Tunnel for Organic Vapors
J. Eng. Gas Turbines Power (May,2016)
Related Proceedings Papers
Related Chapters
Pool Boiling
Thermal Management of Microelectronic Equipment, Second Edition
Thermodynamic Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential