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.