Search Results - "Sipatov, A. M."
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Direct Simulation of Thermoacoustic Instability in Gas Generators Using the CABARET Scheme
Published in Mathematical models and computer simulations (01-09-2021)“…It is shown that the nondissipative CABARET scheme can be used to find the conditions for the occurrence of thermoacoustic instability (vibrational combustion)…”
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Journal Article -
2
The Numerical Simulation of the Atomization of a Kerosene Film in an Air-Assist Atomizer with a Prefilmer
Published in Journal of applied mechanics and technical physics (01-12-2020)“…Using the volume of fluid (VOF) method in the approximation of 2D axisymmetric swirling flow, the primary atomization of a kerosene film in an air-assist…”
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Journal Article -
3
Low-Emission Operation of Aeroderivative Gas-Turbine Combustor over a Wide Range of Ambient Conditions
Published in Power technology and engineering (01-05-2020)“…The capabilities of controlling a low-emission combustor (LEC) over a wide range of ambient conditions are analyzed. The LES is intended for a GTU-16P gas…”
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4
GT-16 Gas Turbine Low-Emission Combustor: Results of Tests in a Single-Burner Chamber on the Stagnation Property Test Facility
Published in Power technology and engineering (2021)“…This paper presents the comprehensive test results of gas turbine unit (GTU-16P) experimental low-emission combustor (LEC) investigations at pressures up to…”
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5
A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
Published in Russian aeronautics (2017)“…A technique for calculating the two-phase flows in the pneumatic injector of the aircraft engine is developed based on solving the model problem, namely, on…”
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6
Structural optimization of the air-blast atomizer based on three-dimensional simulation techniques
Published in Russian aeronautics (2014)“…The experience gained in structural modifying the low-pressure drop gas turbine engine fuel atomizer with two air nozzles is presented. The volume of fluid…”
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7
Investigation of gas dynamics numerical schemes based on the solution of one-dimensional test problems
Published in Russian aeronautics (01-12-2010)“…The application of the optimized dispersion relation preserving scheme (DRP-scheme) in combination with the explicit optimized two-layer Runge-Kutta scheme is…”
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8
Application of high-order accurate methods to solve the computational gas dynamics and aeroacoustics problems
Published in Russian aeronautics (01-03-2011)“…The application of the low dissipative high-order accurate scheme for numerical solution of the Euler and Navier-Stokes equations in the two-dimensional…”
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9
Computation of design parameters influence on air injector fuel atomization
Published in Russian aeronautics (01-07-2017)“…A technique for calculating the two-phase flows at liquid fuel atomization by the air injector is developed. In the course of numerical experiments, the flow…”
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10
Identification of Molecular Bands in Plasma Radiation Spectra Inside a Low-Emission Combustion Chamber
Published in Optoelectronics, instrumentation, and data processing (01-07-2020)“…Molecular bands OH (306.1 nm), CH (430.18 nm), H O (714–980 nm), C (515.55 nm), NH (336 nm), NO (358.26 nm) have been identified (the most intense edges are…”
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Journal Article -
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Fluid film break-up modeling using adaptive mesh refinement models
Published in Russian aeronautics (01-07-2016)“…Numerical modelling of fluid film break-up is carried out using adaptive mesh models. The results obtained are compared with experimental data. It is shown…”
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Journal Article -
12
Experimental investigation of the combustion of a pre-vaporated surrogate of aviation kerosene in a lab-scale combustion chamber
Published in 2021 International Scientific and Technical Engine Conference (EC) (23-06-2021)“…The main purpose of this work is to conduct experimental studies of the combustion of a pre-prepared mixture of aviation kerosene and its surrogate with air…”
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Conference Proceeding -
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Development of Aviation Kerosene TS-1 Surrogate by Combustion Characteristics
Published in 2021 International Scientific and Technical Engine Conference (EC) (23-06-2021)“…This paper presents results of the development of an aviation kerosene TS-1 surrogate in terms of combustion characteristics. The paper briefly shows the…”
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Conference Proceeding