TY - JOUR
T1 - Combustion of single droplets and droplet pairs in a vibrating field under microgravity
AU - Okai, K.
AU - Moriue, O.
AU - Araki, M.
AU - Tsue, M.
AU - Kono, M.
AU - Sato, J.
AU - Dietrich, D. L.
AU - Williams, F. A.
N1 - Funding Information:
This work was performed in part under the management of the Japan Space Utilization Promotion Center under a part of the research and development project of the Advanced Combustion Technologies for Various Fuel supported by the New Energy and Industrial Technology Development Organization. FAW acknowledges the support of the NASA Glenn Research Center through grant no. NAG-1689 in the microgravity science program. DLD thanks U. Hegde for his helpful discussions regarding acoustic effects. We thank Y. Ono and S. Mori for their assistance during the experiment.
PY - 2000
Y1 - 2000
N2 - This paper presents results of an experimental investigation on acoustic effects on combustion of single droplets and droplet pairs in microgravity. The ambient gas was air at atmospheric temperature and pressure, with octane as the fuel. A loudspeaker at the bottom of the chamber produced the acoustic field. Experimental results of single droplets showed that at low frequency and small to moderate acoustic intensities the evaporation rate increases, and the burning rate constant is nearly proportional to the product of frequency, f, and square of displacement, X2a, fX2a. At higher acoustic intensities, the burning rate constant either remains constant or decreases, and, in some cases, flame extinction occurs at a finite droplet diameter. The burning rate constant for a droplet pair is consistently lower than that for a single droplet. At lower frequencies, the burning rate constant reaches a maximum at an intermediate acoustic intensity. At higher frequencies, the burning rate constant increases monotonically with increasing acoustic intensity. Theflame size decreases as a result of interactions, as does the critical spacing that indicates a merged flame around the droplet pair versus individual flames surrounding the droplets. The results also show that interactions stabilize the flame, in that droplet pairs burn to completion under conditions in which the flame surrounding a single droplet extinguishes at a finite droplet diameter.
AB - This paper presents results of an experimental investigation on acoustic effects on combustion of single droplets and droplet pairs in microgravity. The ambient gas was air at atmospheric temperature and pressure, with octane as the fuel. A loudspeaker at the bottom of the chamber produced the acoustic field. Experimental results of single droplets showed that at low frequency and small to moderate acoustic intensities the evaporation rate increases, and the burning rate constant is nearly proportional to the product of frequency, f, and square of displacement, X2a, fX2a. At higher acoustic intensities, the burning rate constant either remains constant or decreases, and, in some cases, flame extinction occurs at a finite droplet diameter. The burning rate constant for a droplet pair is consistently lower than that for a single droplet. At lower frequencies, the burning rate constant reaches a maximum at an intermediate acoustic intensity. At higher frequencies, the burning rate constant increases monotonically with increasing acoustic intensity. Theflame size decreases as a result of interactions, as does the critical spacing that indicates a merged flame around the droplet pair versus individual flames surrounding the droplets. The results also show that interactions stabilize the flame, in that droplet pairs burn to completion under conditions in which the flame surrounding a single droplet extinguishes at a finite droplet diameter.
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U2 - 10.1016/S0082-0784(00)80304-5
DO - 10.1016/S0082-0784(00)80304-5
M3 - Conference article
AN - SCOPUS:84915751650
SN - 1540-7489
VL - 28
SP - 977
EP - 983
JO - Proceedings of the Combustion Institute
JF - Proceedings of the Combustion Institute
IS - 1
T2 - 30th International Symposium on Combustion
Y2 - 25 July 2004 through 30 July 2004
ER -