Numerical Simulation of a Supersonic Ejector for Vacuum Generation with Explicit and Implicit Solver in Openfoam
Ll Macia,
R. Castilla,
P. J. Gamez-Montero,
S. Camacho and
E. Codina
Additional contact information
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
Energies, 2019, vol. 12, issue 18, 1-17
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.
Keywords: supersonic vacuum ejector; vacuum generator; open source; Python; computational fluid dynamics; CFD; compressible density-based; HiSA; rhoCentralFoam; OpenFOAM (search for similar items in EconPapers)
JEL-codes: Q Q0 Q4 Q40 Q41 Q42 Q43 Q47 Q48 Q49 (search for similar items in EconPapers)
Date: 2019
References: View references in EconPapers View complete reference list from CitEc
Citations: View citations in EconPapers (2)
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