| Numerical study of operational processes in a GOx-kerosene rocket engine with liquid film cooling EA Strokach, IN Borovik, VG Bazarov, OJ Haidn Propulsion and Power Research 9 (2), 132-141, 2020 | 17 | 2020 |
| Модернизация испытательного огневого стенда для исследования рабочих процессов в жидкостных ракетных двигателях малых тяг на экологически чистых компонентах топлива АГ Воробьев, ИН Боровик, АН Хохлов, ММ Лизуневич, СА Сокол, ... Вестник Московского авиационного института 17 (1), 14-14, 2010 | 12 | 2010 |
| Simulation of the GOx/GCH4 multi-element combustor including the effects of radiation and algebraic variable turbulent prandtl approaches E Strokach, I Borovik, O Haidn Energies 13 (19), 5009, 2020 | 9 | 2020 |
| Simulation of a gox-gch4 rocket combustor and the effect of the geko turbulence model coefficients E Strokach, V Zhukov, I Borovik, A Sternin, OJ Haidn Aerospace 8 (11), 341, 2021 | 8 | 2021 |
| Development liquid rocket engine of small thrust with combustion chamber from carbon-ceramic composite material AA Kozlov, AG Vorobiev, IN Borovik, IS Kazennov, AV Lahin, ... Nanocomposites with Unique Properties and Applications in Medicine and …, 2011 | 8 | 2011 |
| Математическая модель оценки массовых характеристик кислородно-водородного безгенераторного жидкостно-ракетного двигателя по его основным проектным параметрам ИН Боровик, АА Козлов Труды МАИ, 5, 2008 | 8 | 2008 |
| Liquid rocket engines functional diagnostics system in real-time mode PS Levochkin, DS Martirosov, SS Kamenskii, AA Kozlov, IN Borovik, ... Aerospace MAI Journal 26 (2), 147-154, 2019 | 7 | 2019 |
| Numerical simulation of kerosene dispersion process by the centrifugal atomizer EA Strokach, IN Borovik Vestn. Mosk. Gos. Tekh. Univ. im. NE Baumana, Mashinostr, 37-54, 2016 | 7 | 2016 |
| Determination method of optimum main design parameters of LOx-LH2 ex-pander-cycle LRE for reusable OTV (orbital transfer ve-hicle)[Electronic resource]: rep. to the. 60th Intern IN Borovik, AA Kozlov As-tronautical Cong. Daejeon, 2009 | 7 | 2009 |
| Разработка жидкостного ракетного двигателя малой тяги, работающего на перекиси водорода и керосине АГ Воробьев, ИН Боровик, ХС Уп Сибирский аэрокосмический журнал, 121-126, 2011 | 6 | 2011 |
| Mathematical modeling of heat transfer processes in a wall with a regular pseudo-pore structure P Starikov, A Ionov, S Seliverstov, I Borovik, A Matushkin Proceedings of International Conference on Aerospace System Science and …, 2019 | 5 | 2019 |
| Influence of polyisobutylene kerosene additive on combustion efficiency in a liquid propellant rocket engine I Borovik, E Strokach, A Kozlov, V Gaponov, V Chvanov, P Levochkin, ... Aerospace 6 (12), 129, 2019 | 4 | 2019 |
| Influence of the turbulent Prandtl number on numerical simulation reaction flow IN Borovik, EA Strokach, NS Severina AIP Conference Proceedings 2181 (1), 2019 | 4 | 2019 |
| Predicting the frequency of combustion instability using the measured reflection coefficient through acoustic excitation J Bae, J Yoon, S Joo, J Kim, C Jeong, CH Sohn, IN Borovik, Y Yoon International Journal of Aeronautical and Space Sciences 18 (4), 797-806, 2017 | 4 | 2017 |
| Numerical Study of the Influence of Turbulent Diffusion Coefficients and Turbulent Prandtl Number on the Reactive Flow Simulation in a Combustor VP Zhukov, IN Borovik, EA Strokach Russian Aeronautics 63, 713-720, 2020 | 3 | 2020 |
| Numerical Study of the Injection Parameters Impact on the Efficiency of a Liquid Rocket Engine YS Chudina, EA Strokach, IN Borovik, VY Gidaspov Advances in Theory and Practice of Computational Mechanics: Proceedings of …, 2020 | 3 | 2020 |
| Variety of gas-dynamic turbulent configurations at internal flow in channels of structurally complex bodies Y Kochetkov, I Borovik, O Podymova, A Protopopov IOP Conference Series: Materials Science and Engineering 779 (1), 012030, 2020 | 3 | 2020 |
| Optimization of Liquid Rocket propulsion system for Reusable Orbital Transfer Vehicle I Borovik, D Borovikov, A Protopopov IOP Conference Series: Materials Science and Engineering 589 (1), 012002, 2019 | 3 | 2019 |
| Developing LRE of low thrust using propellants: strong hydrogen peroxide with kerosene AG Vorobiev, IN Borovik, SU Ha Siberian Aerospace Journal 12 (4), 121-126, 2011 | 3 | 2011 |
| Main lines of development of thrusters for reactive control systems of upper stage and spacecrafts AA Kozlov, IA Bazanova, AG Vorobiev, IN Borovik ISSP, 200 7, 2007 | 3 | 2007 |
