Výsledky vyhledávání - "Roman Ivanovitch Savonov"

Akademický článek

An Open-source Solver to Model the Catalytic Decomposition of Monopropellants for Space Thrusters

Autor: Jenny Robledo Asencio, Roman Ivanovitch Savonov, Rodrigo Intini Marques

Publikováno v: Journal of Aerospace Technology and Management, Vol 12, Iss 1 (2020)

This paper presents a solver for the CFD (computational fluid dynamics) modeling of catalytic chambers in monopropellant thrusters based on the open-source OpenFOAM® (Open Field Operation and Manipulation) framework. A model was formulated and used

Externí odkaz: https://doaj.org/article/477eb1a87efe4c4d9f85a48a5a9fbd7b

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Dissertation/ Thesis

Análise numérica e teórica de injetores tipo 'swirl' empregados em motores-foguete a propelente líquido

Autor: Roman Ivanovitch Savonov

Publikováno v: Biblioteca Digital de Teses e Dissertações do ITAInstituto Tecnológico de AeronáuticaITA.

Esta tese apresenta uma investigação detalhada dos injetores centrífugos utilizados para atomização de propelentes líquidos. Inicialmente foram analisadas e comparadas as teorias aplicadas aos cálculos analíticos das dimensões do injetor e d

Externí odkaz: http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1992

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An Open-source Solver to Model the Catalytic Decomposition of Monopropellants for Space Thrusters

Autor: Rodrigo Intini Marques, Roman Ivanovitch Savonov, Jenny Robledo Asencio

Publikováno v: Journal of Aerospace Technology and Management, Vol 12, Iss 1, Pp 1120-1120 (2020)
Journal of Aerospace Technology and Management v.12 2020
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cbf57ce6cdb3213ee08a3e00369a4b9b
http://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e1120.pdf

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Dynamics of the Internal Flow in Swirl Atomizers by CFD Simulations

Autor: Roman Ivanovitch Savonov

This work presents the simulation of the internal flow in a swirl atomizer. The geometry of the atomizer is calculated by analytical equations used in engineering. The numerical simulation of the two-phase flow is performed by using two equations k-�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d5127ec77538c494dd8283540aff5f88
https://doi.org/10.4018/978-1-5225-2903-3.ch005

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The elimination of excessive vibration presented by Altitude Simulation Test Facility for low thrust rocket engines

Autor: Aguinaldo Martins Serra Junior, Roman Ivanovitch Savonov, José Nivaldo Hinckel

Publikováno v: 23rd ABCM International Congress of Mechanical Engineering.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f1bd120d0ec2a0b75aa79b7819bbcd52
https://doi.org/10.20906/cps/cob-2015-1685

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