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Numerical Simulation of a Supersonic Ejector for Vacuum Generation with Explicit and Implicit Solver in Openfoam

Author

Listed:
  • Ll Macia

    (AR Vacuum, Sant Joan Despí, ES-08970 Catalunya, Spain)

  • R. Castilla

    (LABSON—Department of Fluid Mechanics, Universitat Politecnica de Catalunya, Terrassa, ES-08222 Catalunya, Spain)

  • P. J. Gamez-Montero

    (LABSON—Department of Fluid Mechanics, Universitat Politecnica de Catalunya, Terrassa, ES-08222 Catalunya, Spain)

  • S. Camacho

    (AR Vacuum, Sant Joan Despí, ES-08970 Catalunya, Spain)

  • E. Codina

    (LABSON—Department of Fluid Mechanics, Universitat Politecnica de Catalunya, Terrassa, ES-08222 Catalunya, Spain)

Abstract

Supersonic ejectors are used extensively in all kind of applications: compression of refrigerants in cooling systems, pumping of volatile fluids or in vacuum generation. In vacuum generation, also known as zero-secondary flow, the ejector has a transient behaviour. In this paper, a numerical and experimental research of a supersonic compressible air nozzle is performed in order to investigate and to simulate its behaviour. The CFD toolbox OpenFOAM 6 was used, with two density-based solvers: explicit solver rhoCentralFoam, which implements Kurganov Central-upwind schemes, and implicit solver HiSA, which implements the AUSM+up upwind scheme. The behaviour of the transient evacuation ranges between adiabatic polytropic exponent at the beginning of the process and isothermal at the end. A model for the computation of the transient polytropic exponent is proposed. During the evacuation, two regimes are encountered in the second nozzle. In the supercritic regime, the secondary is choked and sonic flow is reached. In the subcritic regime, the secondary flow is subsonic. The final agreement is good with the two different solvers, although simulation tends to slightly overestimate flow rate for large values region.

Suggested Citation

  • Ll Macia & R. Castilla & P. J. Gamez-Montero & S. Camacho & E. Codina, 2019. "Numerical Simulation of a Supersonic Ejector for Vacuum Generation with Explicit and Implicit Solver in Openfoam," Energies, MDPI, vol. 12(18), pages 1-17, September.
    • Handle: RePEc:gam:jeners:v:12:y:2019:i:18:p:3553-:d:267920
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    References listed on IDEAS

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    1. Kumar, Vikas & Sachdeva, Gulshan, 2018. "1-D model for finding geometry of a single phase ejector," Energy, Elsevier, vol. 165(PA), pages 75-92.
    2. Sierra-Pallares, José & García del Valle, Javier & Paniagua, Jorge Muñoz & García, Javier & Méndez-Bueno, César & Castro, Francisco, 2018. "Shape optimization of a long-tapered R134a ejector mixing chamber," Energy, Elsevier, vol. 165(PA), pages 422-438.
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    Cited by:

    1. Llorenç Macia & Robert Castilla & Pedro Javier Gamez-Montero & Gustavo Raush, 2022. "Multi-Factor Design for a Vacuum Ejector Improvement by In-Depth Analysis of Construction Parameters," Sustainability, MDPI, vol. 14(16), pages 1-16, August.
    2. Yongseok Jeon & Hoon Kim & Jae Hwan Ahn & Sanghoon Kim, 2020. "Effects of Nozzle Exit Position on Condenser Outlet Split Ejector-Based R600a Household Refrigeration Cycle," Energies, MDPI, vol. 13(19), pages 1-12, October.

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