Journal
PROCEEDINGS OF THE COMBUSTION INSTITUTE
Volume 34, Issue -, Pages 2221-2228Publisher
ELSEVIER SCIENCE INC
DOI: 10.1016/j.proci.2012.06.129
Keywords
Aluminum; Ice; Combustion; Nano-particles; ALICE
Funding
- Air Force Office of Scientific Research (AFOSR)
- NASA [FA9550-11-1-0002]
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Flame propagation of aluminum-ice (ALICE) mixtures is studied theoretically and experimentally. Both a mono distribution of nano aluminum particles and a bimodal distribution of nano-and micron-sized aluminum particles are considered over a pressure range of 1-10 MPa. A multi-zone theoretical framework is established to predict the burning rate and temperature distribution by solving the energy equation in each zone and matching the temperature and heat flux at the interfacial boundaries. The burning rates are measured experimentally by burning aluminum-ice strands in a constant-volume vessel. For stoichiometric ALICE mixtures with 80 nm particles, the burning rate shows a pressure dependence of r(b) = aP(n), with an exponent of 0.33. If a portion of 80 nm particles is replaced with 5 and 20 mu m particles, the burning rate is not significantly affected for a loading density up to 15-25% and decreases significantly beyond this value. The flame thickness of a bimodal-particle mixture is greater than its counterpart of a mono-dispersed particle mixture. The theoretical and experimental results support the hypothesis that the combustion of aluminum-ice mixtures is controlled by diffusion processes across the oxide layers of particles. (C) 2012 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
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