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Effects of Gas-Phase Radiation and Detailed Kinetics on the Burning and Extinction of a Solid FuelThis is the first attempt to analyze both radiation and detailed kinetics on the burning and extinction of a solid fuel in a stagnation-point diffusion flame. We present a detailed and comparatively accurate computational model of a solid fuel flame along with a quantitative study of the kinetics mechanism, radiation interactions, and the extinction limits of the flame. A detailed kinetics model for the burning of solid trioxane (a trimer of formaldehyde) is coupled with a narrowband radiation model, with carbon dioxide, carbon monoxide, and water vapor as the gas-phase participating media. The solution of the solid trioxane diffusion flame over the flammable regime is presented in some detail, as this is the first solution of a heterogeneous trioxane flame. We identify high-temperature and low-temperature reaction paths for the heterogeneous trioxane flame. We then compare the adiabatic solution to solutions that include Surface radiation only and gas-phase and surface radiation using a black surface model. The analysis includes discussion of detailed flame chemistry over the flammable regime and, in particular, at the low stretch extinction limit. We emphasize the low stretch regime of the radiatively participating flame, since this is the region representative of microgravity flames. When only surface radiation is included, two extinction limits exist (the blow-off limit, and the low stretch radiative limit), and the burning rate and maximum flame temperatures are lower, as expected. With the inclusion of surface and gas-phase radiation, results show that, while flame temperatures are lower, the burning rate of the trioxane diffusion flame may actually increase at low stretch rate due to radiative feedback from the flame to the surface.
Document ID
20010066768
Acquisition Source
Glenn Research Center
Document Type
Technical Publication (TP)
Authors
Rhatigan, Jennifer L.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2001
Subject Category
Propellants And Fuels
Report/Patent Number
NASA/TP-2001-210770
NAS 1.60:210770
S-879
JSC-CN-6843
Report Number: NASA/TP-2001-210770
Report Number: NAS 1.60:210770
Report Number: S-879
Report Number: JSC-CN-6843
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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