The problem of combustion instability in liquid rocket engines by Samir Vekilov, Volodymyr Lipovskyi, Roman Pustovyi

Subjects: “…liquid propellant rocket engines…”
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Analysis of Acoustic Cavitation Surge in a Rocket Engine Turbopump by Hideaki Nanri, Hiroki Kannan, Naoki Tani, Yoshiki Yoshida

“…In a liquid rocket engine, cavitation in an inducer of a turbopump sometimes causes instability phenomena when the inducer is operated at low inlet pressure. …”
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Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine by Xinyou Shan, Yingkun Li, Xiong Chen, Yan Wu, Yong He, Weixuan Li

“…Pasty rocket engines have broad application prospects in the aerospace field. …”
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Mathematical model for heat transfer in variable thickness fins for rocket engines by Volodymyr Sliusariev, Valerii Bucharskyi

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Analysis of properties of inertia regulator of thrust control system of liquid rocket engine by M. M. Dron, A. B. Yakovlev

“…The article presents a mathematical model of a controller with an inertial booster of a liquid-propellant rocket engine, identifies parameters and values that affect its accuracy, and considers measures to reduce static error…”
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FREQUENCY PREDICTION OF STAGED COMBUSTION ROCKET ENGINE BASED ON RBF NEURAL NETWORK by DU FeiPing, TAN YongHua, CHEN JianHua

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Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process by D. A. Savchin, V. P. Nazarov

“…The paper describes the model of the centrifugal pump head curve obtaining process which helps in consideration of the implementation of automated systems in liquid-propellant rocket engine manufacturing. The work contains the simulation of automated and non-automated head curve obtaining. …”
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Trihybrid nanofluid flow through nozzle of a rocket engine: Numerical solution and irreversibility analysis by Basharat Ullah, Rabia Rehman, Hafiz Abdul Wahab, Umar Khan, Walid Emam

“…Research Problem: The research investigates the process of heat transmission and the production of entropy within the regenerative cooling channel of a rocket engine. The primary focus of the investigation is on the use of nanoparticles (titanium dioxide, copper oxide, and alumina dioxide) that are dispersed in water as the base fluid. …”
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Development of mathematical model of processes in gas generator with unitary fuel for powering turbine of liquid rocket engine by A. B. Yakovlev

“…The article considers the dynamic model of a gas generator with control throttle of liquid rocket engine with pumping supply system and unitary fuel for powering the turbine. …”
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Transient spray combustion characteristics in a gas–liquid pintle rocket engine under acoustic excitation by Xuan Jin, Chao Zhu, Dejiang Chen, Zhongpei Zhang

“…Abstract In order to investigate the acoustic oscillation characteristics of gas–liquid pintle rocket engines and elucidate the path by which spray combustion process provides energy to the combustor pressure oscillation, a LOX/GCH4 pintle engine with rectangular combustor was designed. …”
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Design of modernized test bench for analysis of cooling systems with intensification under inertial forces field by V. V. Shalay, K. V. Shcherban

Subjects: “…liquid rocket engines…”
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Experimental study of cooling systems with intensification in field of inertial forces by V. V. Shalay, K. V. Shcherban

Subjects: “…liquid rocket engines…”
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Statement of the problem of designing a liquid rocket engine dual bell nozzle of the maximum thrust using the direct method of the calculus of variations by Ivan Dubrovskyi, Valerii Bucharskyi

“… A rocket engine with a standard single-section profiled nozzle provides maximum thrust only at a certain value of atmospheric pressure [1]. …”
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Numerical Investigation of the Effect of Equivalent Ratio on Detonation Characteristics and Performance of CH₄/O₂ Rotating Detonation Rocket Engine by Xiao Xu, Qixiang Han, Yining Zhang

“…Equivalent ratio (ER) is an important factor affecting detonation characteristics and propulsion performance of rotating detonation rocket engine (RDRE). In this paper, the effects of different equivalent ratios detonation characteristics and thrust performance of methane-oxygen RDRE were studied by 2D numerical simulation. …”
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A Concept for Striking Range Improvement of the GROM/PIORUN Man-Portable Air-Defence System by Krzysztof MOTYL, Mirosław MAKOWSKI, Bogdan ZYGMUNT, Zbigniew PUZEWICZ, Janusz NOGA

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Investigation of properties of system of automatic control of liquid-propellant rocket propulsion system with integrating regulator by I. A. Kyzmenko, A. B. Yakovlev

Subjects: “…liquid rocket engine…”
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Effect of Receiver Holes on Flow and Heat Transfer Characteristics in A Radial Pre-swirl System: A LES Study by D. Wang, C. Song, C. Qiu, W. Wang, Y. Xu, P. I. Mihailovich

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Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization by Mykhailo Vorobei, Mykola Bondarenko

“…The system aims to improve hybrid rocket engine efficiency and reliability by stabilizing oxidizer tank pressure. …”
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The Application of Counter-Rotating Turbine in Rocket Turbopump by Tang Fei, Zhao Xiaolu, Xu Jianzhong

“…This unconventional configuration meets the requirements of turbopump and may benefit the performance and reliability of rocket engines.…”
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Recent Experimental Efforts on High-Pressure Supercritical Injection for Liquid Rockets and Their Implications by Bruce Chehroudi

“…For example, in cryogenic hydrogen/oxygen liquid rocket engines, such as Space Shuttle Main Engine (SSME) or Vulcain (Ariane 5), the injected liquid oxygen finds itself in a supercritical condition. …”
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