TY - JOUR
T1 - Combustion of JP-10-based slurry with Nanosized aluminum additives
AU - Luo, Yu
AU - Xu, Xu
AU - Zou, Ji Jun
AU - Zhang, Xiangwen
N1 - Publisher Copyright:
Copyright © 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2016
Y1 - 2016
N2 - Nanosized aluminum (16% by weight) was added into JP-10 and surfactant (2% by weight) was used to reduce the agglomeration of nanoparticles. Combustion of metalized fuel, as well as pure JP-10, was carried out in a small-scale combustor. The oxygen-to-fuel ratios were set tobe1.7, 1.8, and 1.9, respectively. Anadditional trialofwater injection during combustion was also tested. The pressures at the combustion chamber and nozzle exit, along with the thrust, were measured during the combustion; and intervals of true values of the specific impulse were presented. The results showed that a relatively higher combustion efficiency was achieved with JP-10-based slurry by 3.0 to 9.0% when compared to pure JP-10. However, the specific impulse could be increased only when the combustion-induced heat release was improved enough to overcome the two-phase loss. Depositions at different positions were collected after combustion for deep analysis; and the results of the x-ray diffraction, thermogravimetry analysis, scanning electron microscope, and laser light scattering were presented. A relatively high oxidation rate of the aluminum was obtained in tests without water injection, and the solid particles were mainly spherical and in dimensions of 100-300 nm. In the tests with water injection, stable combustion and increased thrust were achieved; whereas the combustion efficiency and specific impulse were deceased. And, the size of the particles was increased due to the addition of water.
AB - Nanosized aluminum (16% by weight) was added into JP-10 and surfactant (2% by weight) was used to reduce the agglomeration of nanoparticles. Combustion of metalized fuel, as well as pure JP-10, was carried out in a small-scale combustor. The oxygen-to-fuel ratios were set tobe1.7, 1.8, and 1.9, respectively. Anadditional trialofwater injection during combustion was also tested. The pressures at the combustion chamber and nozzle exit, along with the thrust, were measured during the combustion; and intervals of true values of the specific impulse were presented. The results showed that a relatively higher combustion efficiency was achieved with JP-10-based slurry by 3.0 to 9.0% when compared to pure JP-10. However, the specific impulse could be increased only when the combustion-induced heat release was improved enough to overcome the two-phase loss. Depositions at different positions were collected after combustion for deep analysis; and the results of the x-ray diffraction, thermogravimetry analysis, scanning electron microscope, and laser light scattering were presented. A relatively high oxidation rate of the aluminum was obtained in tests without water injection, and the solid particles were mainly spherical and in dimensions of 100-300 nm. In the tests with water injection, stable combustion and increased thrust were achieved; whereas the combustion efficiency and specific impulse were deceased. And, the size of the particles was increased due to the addition of water.
UR - https://www.scopus.com/pages/publications/84983622391
U2 - 10.2514/1.B35969
DO - 10.2514/1.B35969
M3 - 文章
AN - SCOPUS:84983622391
SN - 0748-4658
VL - 32
SP - 1167
EP - 1177
JO - Journal of Propulsion and Power
JF - Journal of Propulsion and Power
IS - 5
ER -