Skip to main content
U.S. flag

An official website of the United States government

Official websites use .gov
A .gov website belongs to an official government organization in the United States.

Secure .gov websites use HTTPS
A lock ( ) or https:// means you’ve safely connected to the .gov website. Share sensitive information only on official, secure websites.

Numerical and Experimental Studies of Extinguishment of Cup-Burner Flames by C6F12O

Published

Author(s)

Fumiaki Takahashi, Viswanath R. Katta, Valeri I. Babushok, Gregory T. Linteris

Abstract

The extinguishment processes of cup-burner flames by adding a halon-replacement fire-extinguishing agent C6F12O (Novec 1230) to coflowing air in normal gravity have been studied computationally and experimentally. The time-dependent, axisymmetric numerical simulations with a detailed reaction mechanism (up to 141 species and 2206 reactions), molecular diffusive transport, and a gray-gas radiation model, reveal a unique two-zone flame structure. The peak reactivity spot (i.e., reaction kernel) at the flame base stabilizes a trailing flame, which is inclined inwardly by a buoyancy-induced entrainment flow. As the volume fraction of the agent in the coflow air is increased gradually, the total heat release increases up to three times due to the additional exothermic reactions to form HF and CF2O, thus resulting in a two-zone diffusion flame structure; whereas at the base, the flame-anchoring reaction kernel weakens (the local heat release rate decreases) and eventually the flame blows off. A numerical experiment, in which the C6F12O agent decomposition reactions are turned off, indicates that for addition of inert C6F12O, the maximum flame temperature decreases rapidly due to its large heat capacity and the blow-off extinguishment occurs at ≈1700 K, a value identical to that for inert gases previously studied, while the reaction kernel is still burning vigorously. The calculated minimum extinguishing concentrations of C6F12O in a propane flame are 4.2 % (with full chemistry), and 4.3 % (without agent decomposition) which is in fairly good agreement with the measured value of 5.1 %.
Citation
Proceedings of the Combustion Institute
Volume
38
Issue
3

Keywords

Aircraft cargo-bay fire suppression, Halon 1301 replacement, Novec 1230, Diffusion flame stabilization, Reaction kernel

Citation

Takahashi, F. , Katta, V. , Babushok, V. and Linteris, G. (2020), Numerical and Experimental Studies of Extinguishment of Cup-Burner Flames by C6F12O, Proceedings of the Combustion Institute, [online], https://doi.org/10.1016/j.proci.2020.05.053 (Accessed October 3, 2024)

Issues

If you have any questions about this publication or are having problems accessing it, please contact reflib@nist.gov.

Created August 1, 2020, Updated September 26, 2023