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Computational Thermal Sciences: An International Journal

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ISSN Печать: 1940-2503

ISSN Онлайн: 1940-2554

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: 1.5 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: 1 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: 0.3 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: 0.00017 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: 0.28 SJR: 0.279 SNIP: 0.544 CiteScore™:: 2.5 H-Index: 22

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NUMERICAL SIMULATION OF HEAT AND MASS TRANSFER BETWEEN HETEROGENEOUS FLOW AND AN OBSTACLE

Том 3, Выпуск 1, 2011, pp. 15-30
DOI: 10.1615/ComputThermalScien.v3.i1.20
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Краткое описание

This paper describes the problems of numerical simulation of supersonic gas-particle flow over blunt bodies. A complex mathematical model is proposed, coupling gas flow in the shock layer, particle advection in the carrying phase, and heat- mass transfer in the body that is being destroyed. The Eulerian description fits best for the gas phase, and the Lagrangian description is most suitable for the dispersed phase. Particle dynamics is fully handled via the discrete-element method. The result is a numerical simulation of the thermoerosive destruction of a circular cylinder in two-phase flow. The authors present an analysis of multiple factors, such as interparticle collisions in a flow, particle reflection from a streamlined surface, dispersed admixture feedback on the carrier phase, and the influence of changing body geometry due to mass entrainment on two-phase shock layer parameters.

ЦИТИРОВАНО В
  1. Dombrovsky Leonid A., Reviznikov Dmitry L., Sposobin Andrey V., Radiative heat transfer from supersonic flow with suspended particles to a blunt body, International Journal of Heat and Mass Transfer, 93, 2016. Crossref

  2. Reviznikov D. L., Sposobin A. V., Sukharev T. Yu., Numerical simulation of the flow around a blunt body in supersonic polydisperse stream, High Temperature, 55, 3, 2017. Crossref

  3. Reviznikov D. L., Sposobin A. V., Ivanov I. E., A Change in the Structure of a Flow under the Action of Highly Inertial Particle when a Hypersonic Heterogeneous Flow Passes over a Body, High Temperature, 56, 6, 2018. Crossref

  4. Reviznikov Dmitry, Sposobin Andrey, Numerical simulation of supersonic gas flow with binary particle admixture over a blunt body, COMPUTATIONAL MECHANICS AND MODERN APPLIED SOFTWARE SYSTEMS (CMMASS’2019), 2181, 2019. Crossref

  5. Reviznikov D. L., Sposobin A. V., Ivanov I. E., Oscillatory Flow Regimes Resulting from the Shock Layer–Particle Interaction, High Temperature, 58, 2, 2020. Crossref

  6. Sposobin Andrey, Reviznikov Dmitry, Impact of High Inertia Particles on the Shock Layer and Heat Transfer in a Heterogeneous Supersonic Flow around a Blunt Body, Fluids, 6, 11, 2021. Crossref

  7. Sposobin A. V., Reviznikov D. L., Ivanov I. E., Kryukov I. A., Pressure and Heat Flux Oscillations Induced by Gas-Dynamic Interaction between a High Inertia Particle and a Shock Layer, Russian Aeronautics, 63, 4, 2020. Crossref

  8. Reviznikov D. L., Sposobin A. V., Ivanov I. E., Comparative Analysis of Calculated and Experimental Data on an Oscillating Flow Induced by the Gasdynamic Interaction of a Particle with a Shock Layer, High Temperature, 58, 6, 2020. Crossref

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