TY - GEN
T1 - Modeling the diffusion to kinetically controlled burning transition of micron-sized aluminum particles
AU - Bojko, Brian
AU - DesJardin, Paul E.
AU - Washburn, Ephraim B.
N1 - Publisher Copyright:
© 2015 by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2015
Y1 - 2015
N2 - Aluminum particle burn rates are known to be a strong function of particle size as the mode of burning transitions from diffusion to kinetically controlled. To better understand the rate dependent diffusion and kinetic processes, a fully compressible, one-dimensional, spherically symmetric particle burn model is developed. Several cases are studied to explore the burning of aluminum particles in air, carbon-dioxide and steam environments. Predictions of burn rates versus particle size reveal significant deviations from a diffusion controlled burning limit - highlighting the importance of accounting for finite-rate chemistry in modeling the burning of sub-micron aluminum particles. While overall agreement to data is satisfactory, the detailed model cannot be directly used in system level tools due to computational cost. A reduced modeling strategies are therefore explored to account for finite-rate chemistry effects in simpler models for use in system level CFD analysis. An augmented D2 - law where the finite-rate chemistry is treated as a perturbation to flame sheet approximation via augmented burn rate "constants". Predictions using this approach of de agration speeds in dusty aluminum-air gases agree well with experiments and show evidence of a maximum flame speed for a given mass loading.
AB - Aluminum particle burn rates are known to be a strong function of particle size as the mode of burning transitions from diffusion to kinetically controlled. To better understand the rate dependent diffusion and kinetic processes, a fully compressible, one-dimensional, spherically symmetric particle burn model is developed. Several cases are studied to explore the burning of aluminum particles in air, carbon-dioxide and steam environments. Predictions of burn rates versus particle size reveal significant deviations from a diffusion controlled burning limit - highlighting the importance of accounting for finite-rate chemistry in modeling the burning of sub-micron aluminum particles. While overall agreement to data is satisfactory, the detailed model cannot be directly used in system level tools due to computational cost. A reduced modeling strategies are therefore explored to account for finite-rate chemistry effects in simpler models for use in system level CFD analysis. An augmented D2 - law where the finite-rate chemistry is treated as a perturbation to flame sheet approximation via augmented burn rate "constants". Predictions using this approach of de agration speeds in dusty aluminum-air gases agree well with experiments and show evidence of a maximum flame speed for a given mass loading.
UR - https://www.scopus.com/pages/publications/84980413788
U2 - 10.2514/6.2015-0166
DO - 10.2514/6.2015-0166
M3 - Conference contribution
AN - SCOPUS:84980413788
SN - 9781624103438
T3 - 53rd AIAA Aerospace Sciences Meeting
BT - 53rd AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA Aerospace Sciences Meeting, 2015
Y2 - 5 January 2015 through 9 January 2015
ER -