TY - JOUR
T1 - Pressure effects on combustion of methanol and methanol/dodecanol single droplets and droplet pairs in 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 under the management of the Japan Space Utilization Promotion Center (JSUP) as a part of the R&D project of the Advanced Combustion Science Utilizing Microgravity supported by the New Energy and Industrial Technology Development Organization (NEDO). FAW acknowledges the support of the NASA Glenn (formerly Lewis) Research Center through Grant NAG-1689 in the microgravity science program. We thank B.-L. Zhang for his helpful advice concerning the theoretical calculations and Y. Ono for his assistance during the analysis.
PY - 2000/3
Y1 - 2000/3
N2 - This paper presents the results of an experimental investigation on the combustion of single droplets and two-droplet arrays of pure methanol and methanol/dodecanol mixtures in air under microgravity conditions. The initial droplet diameters, d0, were nominally 0.9 mm. The independent experimental variables were the ambient pressure (0.1-9.0 MPa), fuel mixture ratio (methanol/dodecanol: 100/0-15/85), and interdroplet separation distance l (l/d0 = 2.3-8.0). For pure methanol, the results show that the droplet lifetime decreases with increasing interdroplet separation distances at low pressures. At higher pressures (3.0 MPa and above) the droplet lifetime was independent of separation distance. The flame extinguished at a finite droplet size only for pure methanol at 0.1 MPa, in qualitative agreement with theoretical predictions. The extinction droplet diameter was nearly independent of the droplet spacing. Methanol/dodecanol-mixture droplets exhibited microexplosion for both single droplets and droplet arrays. The paper presents maps of the disruption regime for both single droplets and droplet pairs. The difference between the disruptive behavior of single droplets and droplet pairs is explained by differences in liquid-phase circulation induced by the gas-phase asymmetry of the droplet pair. The paper also presents results of the dependence of the onset of disruption (in terms of both volume and time) on the pressure and initial fuel mixture ratio.
AB - This paper presents the results of an experimental investigation on the combustion of single droplets and two-droplet arrays of pure methanol and methanol/dodecanol mixtures in air under microgravity conditions. The initial droplet diameters, d0, were nominally 0.9 mm. The independent experimental variables were the ambient pressure (0.1-9.0 MPa), fuel mixture ratio (methanol/dodecanol: 100/0-15/85), and interdroplet separation distance l (l/d0 = 2.3-8.0). For pure methanol, the results show that the droplet lifetime decreases with increasing interdroplet separation distances at low pressures. At higher pressures (3.0 MPa and above) the droplet lifetime was independent of separation distance. The flame extinguished at a finite droplet size only for pure methanol at 0.1 MPa, in qualitative agreement with theoretical predictions. The extinction droplet diameter was nearly independent of the droplet spacing. Methanol/dodecanol-mixture droplets exhibited microexplosion for both single droplets and droplet arrays. The paper presents maps of the disruption regime for both single droplets and droplet pairs. The difference between the disruptive behavior of single droplets and droplet pairs is explained by differences in liquid-phase circulation induced by the gas-phase asymmetry of the droplet pair. The paper also presents results of the dependence of the onset of disruption (in terms of both volume and time) on the pressure and initial fuel mixture ratio.
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U2 - 10.1016/S0010-2180(99)00160-1
DO - 10.1016/S0010-2180(99)00160-1
M3 - Article
AN - SCOPUS:0033622637
SN - 0010-2180
VL - 121
SP - 501
EP - 512
JO - Combustion and Flame
JF - Combustion and Flame
IS - 3
ER -