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R. К. Seleznev

Observed names: R K Seleznev, R. K. Seleznev, R.K. Seleznev, Roman Seleznev
ORCID: 0000-0003-3047-3848
Observed ORCID: 0000-0003-3047-3848
OpenAlex ID: A5072843540
A review of the scramjet experimental data base
2019 · R.K. Seleznev, S.T. Surzhikov, et al. · Progress in Aerospace Sciences · 151
History of scramjet propulsion development
2018 · R K Seleznev · Journal of Physics Conference Series · 31
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Unsteady Thermo-Gasdynamic Processes in Scramjet Combustion Chamber with Periodical Input of Cold Air
2014 · Sergey Surzhikov, Roman Seleznev, et al. · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · 16
Comparison of two-dimensional and quasi-one-dimensional scramjet models by the example of VAG experiment
2017 · R K Seleznev · Journal of Physics Conference Series · 12
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Validation of 3D model by the example of a supersonic inlet-isolator
2018 · R K Seleznev · Journal of Physics Conference Series · 11
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A Quasi-One-Dimensional Analysis of Hydrogen-Fueled Scramjet Combustors
2016 · Roman Seleznev, Sergey Surzhikov · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 10
Quasi-One-Dimensional and Two-Dimensional Numerical Simulation of Scramjet Combustors
2015 · Roman Seleznev, Sergey Surzhikov · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 10
Analysis of the Flow Structure in a Supersonic Channel with Cavity
2024 · R. K. Seleznev · Fluid Dynamics · 9
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Investigation of the Flow Structure in a Model Scramjet Air Intake with Transverse Hydrogen Fuel Injection into Supersonic Crossflow
2021 · R. K. Seleznev · Fluid Dynamics · 9
Numerical study of the flow structure in the supersonic inlet-isolator
2018 · R K Seleznev · Journal of Physics Conference Series · 9
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Numerical study of the processes of resonance emergence in the experimental set-up of a pulse detonation engine
2014 · Yu. V. Polezhaev, R. K. Seleznev · High Temperature · 9
On the Method for Estimating the Integral Characteristics of a Generic Scramjet with an Integrated Propulsion System
2023 · R. K. Seleznev · Fluid Dynamics · 8
Validation of two-dimensional model by the example of a supersonic inlet-isolator
2018 · R K Seleznev · Journal of Physics Conference Series · 8
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Numerical Investigation of the Ramjet and Scramjet Operation Regimes of the HIFiRE-2 Combustion Chamber
2022 · R. K. Seleznev · Fluid Dynamics · 7
Generalized Newton Method For Solving Differential Equations of Chemical Kinetics
2013 · Roman Seleznev, Sergey Surzhikov · AIAA Thermophysics Conference · 5
Comparison of Ramjet and Scramjet Modes in the Combustion Chamber of the HIFiRE-2 experiment
2021 · R. K. Seleznev · Physical-Chemical Kinetics in Gas Dynamics · 2
The Study of the Flow Structure in the Scramjet Inlet-Isolator with Throttle
2019 · R.K. Seleznev · Physical-Chemical Kinetics in Gas Dynamics · 2
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Development of Helicon Plasma Thruster Model
2017 · Victor Kuzenov, Roman Seleznev, et al. · AIAA/SAE/ASEE Joint Propulsion Conference (JPC) · 1
Analysis of the flow structure in a supersonic channel with cavity
2024 · R. К. Seleznev · Fluid Dynamics
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On the Method for Estimating the Integral Characteristics of a Generic Scramjet with an Integrated Propulsion System
2023 · R. K. Seleznev · Physical-Chemical Kinetics in Gas Dynamics
Approximate Thermal Analysis of Heating and Deformation of a C/C-SiC Plate in a Scramjet Engine
2023 · R. K. Seleznev, V. V. Kuzenov · Physical-Chemical Kinetics in Gas Dynamics
Development of a Method for Assessing Thermal Stresses in Structural Elements of Aircraft
2023 · R. K. Seleznev, V. V. Kuzenov · Physical-Chemical Kinetics in Gas Dynamics
Numerical study of the flow structure in the supersonic inlet-isolator with mechanical throttle
2019 · R K Seleznev · Journal of Physics Conference Series
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Works count: 23
Citation count: 310
H-index: 9
I10-index: 7
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