Loughborough University
Leicestershire, UK
LE11 3TU
+44 (0)1509 263171
Loughborough University

Loughborough University Institutional Repository

Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/28375

Title: A new model based on adiabatic flame temperature for evaluation of the upper flammable limit of alkane-air-CO2 mixtures
Authors: Wu, Mingqiang
Shu, Gequn
Chen, Rui
Tian, Hua
Wang, Xueying
Wang, Yue
Keywords: Flammability limits
Dilution ratio
Theoretical models
Variable calculation adiabatic flame temperature
Experimental method
Issue Date: 2017
Publisher: © Elsevier
Citation: WU, M. ...et al., 2017. A new model based on adiabatic flame temperature for evaluation of the upper flammable limit of alkane-air-CO2 mixtures. Journal of Hazardous Materials, 344, pp. 450-457.
Abstract: © 2017 Elsevier B.V. For security issue of alkane used in Organic Rankine Cycle, a new model to evaluate the upper flammability limits for mixtures of alkanes, carbon dioxide and air has been proposed in present study. The linear relationship was found at upper flammability limits between molar fraction of diluent in alkane-CO 2 mixture and calculated adiabatic flame temperature. The prediction ability of the variable calculated adiabatic flame temperature model that incorporated the linear relationship above is greatly better than the models that adopted the fixed calculated adiabatic flame temperature at upper flammability limit. The average relative differences between results predicted by the new model and observed values are less than 3.51% for upper flammability limit evaluation. In order to enhance persuasion of the new model, the observed values of n-butane-CO 2 and isopentane-CO 2 mixtures measured in this study were used to confirm the validity of the new model. The predicted results indicated that the new model possesses the capacity of practical application and can adequately provide safe non-flammable ranges for alkanes diluted with carbon dioxide.
Description: This paper is in closed access until 17th October 2018.
Sponsor: This work was supported by a grant from the National Natural Science Foundation of China (No. 51676133).
Version: Accepted for publication
DOI: 10.1016/j.jhazmat.2017.10.030
URI: https://dspace.lboro.ac.uk/2134/28375
Publisher Link: https://doi.org/10.1016/j.jhazmat.2017.10.030
ISSN: 0304-3894
Appears in Collections:Closed Access (Aeronautical and Automotive Engineering)

Files associated with this item:

File Description SizeFormat
Chen_Accepted_2017-10-16.pdfAccepted version1.14 MBAdobe PDFView/Open

 

SFX Query

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.