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Heat Transfer Research

Publication de 18  numéros par an

ISSN Imprimer: 1064-2285

ISSN En ligne: 2162-6561

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: 1.7 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: 1.4 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: 0.6 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: 0.00072 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: 0.43 SJR: 0.318 SNIP: 0.568 CiteScore™:: 3.5 H-Index: 28

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INCREASING THE MUZZLE VELOCITY OF PROJECTILE IN THE MODEL BALLISTIC INSTALLATION BY USING HIGH-DENSITY PROPELLANTS

Volume 51, Numéro 13, 2020, pp. 1213-1219
DOI: 10.1615/HeatTransRes.2020034468
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RÉSUMÉ

In accordance with the early works of the authors, the modernization of the propellant charge is possible by using propellant like a traveling charge pushing a projectile in the barrel. The advantages of this technology are increase in the loading density and propellant mass, and therefore increase in the energy of the propellant. The use of this technology leads to the redistribution of the combustion products' energy in the space behind the projectile. In this work, the problem was solved by increasing the throwing velocity while maintaining the maximum pressure on the bore bott om by using high-density propellants in the form of traveling charge at the conditions of the shot for the model ballistic installation. A comparison of the ballistic parameters for the classical shot scheme and scheme with high-density propellants as traveling charge was made.

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