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International Journal of Energetic Materials and Chemical Propulsion

年間 6 号発行

ISSN 印刷: 2150-766X

ISSN オンライン: 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

MODELING OF EVOLUTION OF THE COARSE FRACTION OF CONDENSED COMBUSTION PRODUCTS ON A SURFACE OF BURNING ALUMINIZED PROPELLANT AND WITHIN A COMBUSTION PRODUCTS FLOW

巻 16, 発行 1, 2017, pp. 23-38
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2017021173
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要約

The paper is devoted to generalization of results of theoretical studies of the coarse fraction of condensed combustion products evolution at burning of aluminized solid propellants. The evolution of coarse condensed combustion products is represented by a set of phenomena from emergence and staying of individual agglomerating particles on surface of burning propellant to subsequent agglomerates motion within combustion products flow. Developed models describe the phenomena at the evolution with considering of propellant surface and multiphase flow features. Agglomerating particles evolution on surface of burning propellant is described as a final part of the agglomeration process. For the agglomerates evolution within multiphase flow, the non-uniform flow nature, interactions of agglomerates with gaseous combustion products, and smoke oxide are taken into account. Numerical analysis of developed models was performed. Comparison of modeling and experimental results for a several cases allowed us to make a conclusion about modeling adequacy. The models allow us to determine a set of properties of the coarse condensed combustion products depending on propellant formulation, burning conditions, agglomeration regularities, and geometric configuration of computational region.

によって引用された
  1. Li Jun-Qiang, Liu Linlin, Fu Xiaolong, Tang Deyun, Wang Yin, Hu Songqi, Yan Qi-Long, Transformation of Combustion Nanocatalysts inside Solid Rocket Motor under Various Pressures, Nanomaterials, 9, 3, 2019. Crossref

  2. Babuk Valery A., Budnyi Nikita L., Kuklin Dimitry I., Nizyaev Alexander A., Analysis of multiphase flow evolution influence on properties of condensed phase particles, THERMOPHYSICAL BASIS OF ENERGY TECHNOLOGIES (TBET 2019), 2212, 2020. Crossref

  3. Babuk Valery A., Budnyi Nikita L., Nizyaev Alexander A., Simulation of Condensed Products Formation at the Surface of a Metalized Solid Propellant, in Innovative Energetic Materials: Properties, Combustion Performance and Application, 2020. Crossref

  4. Babuk V. A., Budnyi N. L., Kuklin D. I., Naryzhnyi S. Yu., Nizyaev A. A., Intermediate Structures in the Process of Burning of High-Energy Condensed Systems, Combustion, Explosion, and Shock Waves, 58, 4, 2022. Crossref

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