Published September 2007 | Version v1
Journal article

Shock circle model for ejector performance evaluation

  • 1. School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore 639798 (Singapore)
  • 2. School of Energy and Power Engineering, Xi'an Jiao Tong University, Xi'an 710049 (China)

Description

In this paper, a novel shock circle model for the prediction of ejector performance at the critical mode operation is proposed. By introducing the 'shock circle' at the entrance of the constant area chamber, a 2D exponential expression for velocity distribution is adopted to approximate the viscosity flow near the ejector inner wall. The advantage of the 'shock circle' analysis is that the calculation of ejector performance is independent of the flows in the constant area chamber and diffuser. Consequently, the calculation is even simpler than many 1D modeling methods and can predict the performance of critical mode operation ejectors much more accurately. The effectiveness of the method is validated by two experimental results reported earlier. The proposed modeling method using two coefficients is shown to produce entrainment ratio, efficiency and coefficient of performance (COP) accurately and much closer to experimental results than those of 1D analysis methods

Additional details

Identifiers

DOI
10.1016/j.enconman.2007.03.024;
PII
S0196-8904(07)00095-7;

Publishing Information

Journal Title
Energy Conversion and Management
Journal Volume
48
Journal Issue
9
Journal Page Range
p. 2533-2541
ISSN
0196-8904
CODEN
ECMADL

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
39012304
Subject category
S29: ENERGY PLANNING, POLICY AND ECONOMY;
Descriptors DEI
COEFFICIENT OF PERFORMANCE; DIFFUSERS; EFFICIENCY; ENTRAINMENT; EVALUATION; FORECASTING; PERFORMANCE; REFRIGERATION; SIMULATION
Descriptors DEC
COOLING

Optional Information

Copyright
Copyright (c) 2007 Elsevier Science B.V., Amsterdam, The Netherlands, All rights reserved.