Abstract

In general, engine fuel combustion generates 30% waste heat, which is disposed to the environment. The use of the steam ejector refrigeration to recycle the waste heat and transfer them to useful energy source could be an environmentally friendly solution to such an issue. The steam ejector is the main component of the ejector refrigeration system, which can operate at a low-temperature range. In this article, the internal shock wave structure of the ejector is comprehensively studied through the computation fluid dynamics (CFD) approach. The shock wave structure can be subdivided into two regions: firstly the pseudo-shock region consisting of shock train and co-velocity region; secondly the oblique-shock region composed of a single normal shock and a series of oblique shocks. The effect of the shock wave structure on both pumping performance and the critical back pressure were investigated. Numerical predictions indicated that the entrainment ratio is enhanced under two conditions including (i) a longer pseudo-shock region and (ii) when the normal shock wave occurs near the outlet. Furthermore, the system is stabilized as the back pressure and its disturbance is reduced. A critical range of the primary fluid pressure is investigated such that the pumping is effectively optimized.

Highlights

  • The steam ejector refrigeration system has been well-recognized to be a very promising device in saving energy and reducing and environmental pollution [1]

  • The shock train and the co-velocity region are collectively referred to as a pseudo shock region [43] while the oblique-shock region consisting of a single normal shock wave and a series of oblique shocks [40], and the range of which is from the position of the normal shock wave to the coincidence point C

  • The main findings of this study are as follows: (i) the shock wave structure is thoroughly studied by the experimental-computation fluid dynamics (CFD) method

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Summary

Part 2.

Yu Han 1,2 , Xiaodong Wang 1, *, Lixin Guo 1 , Anthony Chun Yin Yuen 2 , Hengrui Liu 2 , Ruifeng Cao 2 , Cheng Wang 2 , Cuiling Li 1 , Jiyuan Tu 3 and Guan Heng Yeoh 2,4. Australian Nuclear Science and Technology Organization (ANSTO), Locked Bag 2001, Kirrawee DC, NSW 2232, Australia. Received: 17 September 2019; Accepted: 16 October 2019; Published: 19 October 2019

Introduction
Governing Equations
Geometry and Mesh Approach
Numerical solution procedure
Structural Division of Shock Wave Structure in the Ejector
Effect of the shock wave structure on the pumping performance
Effect of the shock wave on the critical back pressure
Conclusions
Full Text
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