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国际能源材料和化学驱动期刊

每年出版 6 

ISSN 打印: 2150-766X

ISSN 在线: 2150-7678

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.7 To calculate the five year Impact Factor, citations are counted in 2017 to the previous five years and divided by the source items published in the previous five years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) 5-Year IF: 0.7 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.1 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00016 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.18 SJR: 0.313 SNIP: 0.6 CiteScore™:: 1.6 H-Index: 16

Indexed in

COMBUSTION CHARACTERISTICS OF KEROSENE CONTAINING ALEX® NANO-ALUMINUM

卷 5, 册 1-6, 2002, pp. 195-205
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.210
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摘要

Aluminum is a highly energetic metal that can react with a wide variety of oxidizers to produce propellants with high specific impulse. When added to kerosene rocket fuel aluminum substantially increases theoretical volumetric density Isp, potentially reducing the size of tankage and overall system weight. However, aluminum tends to agglomerate in burning liquid hydrocarbon droplets delaying combustion within the engine, reducing delivered performance. Gels were formulated of 0, 25, 30 and 55 weight percent Alex® nano aluminum powder in RP-1 (kerosene) using a combination of wetting and gelling agents. The viscosity of such gels was measured as a function of aluminum content, temperature and shear rate and were found to be non-Newtonian, so called yield pseudoplastic. At loadings greater than 30 weight percent Alex® no foreign gellant is necessary to achieve dynamic stability as measured by centrifuging the gels at 1300 rpm for one hour. In contrast, micron size aluminum gels required 5% fumed silica as a gellant to achieve dynamic stability, as did the gels containing 5% Alex®. Ignition delay of Alex®/RP-1 gels were determined in a laboratory bomb over the temperature range 400−600°C and compared to RP-1 gels without any aluminum and to neat RP-1. The data show that nano aluminum could be completely consumed during the interval of spraying in a short laboratory bomb. Moreover, the combustion of Alex® accelerated the ignition of the RP-1.

对本文的引用
  1. Pan Lun, E Xiu‐Tian‐Feng, Cao Jinwen, Xue Kang, Design and Synthesis of Nanofluid Fuels, in High‐Energy‐Density Fuels for Advanced Propulsion, 2020. Crossref

  2. DeLuca Luigi T., A Survey of Nanotechnology for Rocket Propulsion, in The ELSI Handbook of Nanotechnology, 2020. Crossref

  3. DeLuca Luigi T., Pang WeiQiang, Transient Burning of nAl-Loaded Solid Rocket Propellants, in Innovative Energetic Materials: Properties, Combustion Performance and Application, 2020. Crossref

  4. Cao Jinwen, Zhang Yong‐Chao, Pan Lun, Shi Chengxiang, Zhang Xiangwen, Zou Ji‐Jun, Synthesis and Characterization of Gelled High‐Density Fuels with Low‐Molecular Mass Gellant, Propellants, Explosives, Pyrotechnics, 45, 7, 2020. Crossref

  5. Xue Kang, Cao Jinwen, Pan Lun, Zhang Xiangwen, Zou Ji-Jun, Review on design, preparation and performance characterization of gelled fuels for advanced propulsion, Frontiers of Chemical Science and Engineering, 16, 6, 2022. Crossref

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