A Burke-Schumann analysis of dual-flame structure supported by a burning droplet. (October 2017)

• Record Type: Journal Article
• Authors: Nayagam, Vedha; Dietrich, Daniel L.; Williams, Forman A.
• Is Part Of: International communications in heat and mass transfer. Volume 87(2017)
• Page Start: 84
• Page End: 89
• Publication Date: 2017-10
• Subjects: Dual flames -- Cool flames -- Droplet combustion; Heat -- Transmission -- Periodicals; Mass transfer -- Periodicals; Chaleur -- Transmission -- Périodiques; Transfert de masse -- Périodiques; Heat -- Transmission; Mass transfer; Periodicals; 621.4022
• DOI: 10.1016/j.icheatmasstransfer.2017.06.016
• Languages: English
• ISSNs: 0735-1933

Abstract

Abstract: Droplet combustion experiments carried out onboard the International Space Station, using pure fuels and fuel mixtures, have shown that quasi-steady burning can be sustained by a non-traditional flame configuration, namely a "cool flame" burning in the "partial-burning" regime where both fuel and oxygen leak through the low-temperature-controlled flame-sheet. Recent experiments involving large, bi-component fuel ( n -decane and hexanol, 50/50 by volume) droplets at elevated pressures show that the visible, hot flame becomes extremely weak while the burning rate remains relatively high, suggesting the possible simultaneous presence of "cool" and "hot" flames of roughly equal importance. The radiant output from these bi-component droplets is relatively high and cannot be accounted for only by the presence of a visible hot flame. In this analysis we explore the theoretical possibility of a dual-flame structure, where one flame lies close to the droplet surface, called the "cool flame", and the other farther away from the droplet surface, termed the "hot flame". A Burke-Schumann analysis of this dual structure seems to indicate that such flame structures are possible over a limited range of initial conditions. These theoretical results can be compared against available experimental data for pure and bi-component fuel droplet combustion to test how realistic the model may be.