Lyubimov Dmitriy Alexandrovich

Publications in Math-Net.Ru

1. Анализ RANS/ILES(i)-методом влияния турбулентности набегающего потока на течение в сверхзвуковом воздухозаборнике. Различные режимы работы воздухозаборника
   
   TVT, 62:4 (2024),  544–557
2. Особенности моделирования тепломассообменных процессов при формировании льда в условиях атмосферного облака, состоящего из переохлажденных капель
   
   TVT, 62:2 (2024),  250–263
3. Study of vortex-resolving method of throttling effect on pressure pulsation spectra in a paired supersonic air intake
   
   Mat. Model., 35:9 (2023),  61–76
4. Analysis of the influence of incoming flow turbulence on the flow in a supersonic air intake by the RANS/ILES method. Estimation of dissipative properties of the difference scheme by an example of modeling the decay of homogeneous isotropic turbulence in the ILES
   
   TVT, 60:1 (2022),  63–75
5. Study by the RANS/ILES method throttling influence on pressure pulsations in a multiple-module supersonic air intake
   
   Mat. Model., 33:7 (2021),  63–78
6. A RANS/ILES study of the features of the flow in the spatial air intake of a supersonic business-class aircraft in throttle modes
   
   TVT, 59:4 (2021),  576–583
7. Use of the RANS/ILES method to study the efficiency of synthetic jet application for flow control in an S-shaped intake integrated with an airframe
   
   TVT, 58:2 (2020),  287–299
8. Analysis by RANS/ILES method the influence of variable heat capacity on the characteristics of pressure pulsations in a high-speed air intake
   
   Mat. Model., 31:10 (2019),  72–86
9. Study of temperature field non-uniformity influence on pressure pulsations in inlet duct using RANS/ILES-method
   
   Mat. Model., 31:10 (2019),  35–48
10. Study of the possibilities of gasdynamic air flow control in the spatial air intake of a light supersonic business-class aircraft by the RANS/ILES method
    
    TVT, 57:1 (2019),  127–136
11. Flow in a high-velocity mixed compression inlet studied by the RANS/ILES method in different operation modes
    
    TVT, 56:5 (2018),  729–737
12. The use of the RANS/ILES method to study the influence of coflow wind on the flow in a hot, nonisobaric, supersonic airdrome jet during its interaction with the jet blast deflector
    
    TVT, 56:2 (2018),  261–269
13. A study of unsteady-state operating conditions of a supersonic inlet by the RANS/ILES method
    
    TVT, 54:5 (2016),  784–791
14. Investigation of the effect of a pylon and a wing with flaps on the flow within an exhaust jet of a double-flow turbojet engine by a simulation method for large eddies
    
    TVT, 51:1 (2013),  120–137
15. Development and application of a high-resolution technique for jet flow computation using large eddy simulation
    
    TVT, 50:3 (2012),  450–466
16. Investigation of Impact of Jets with Zero-Net-Mass Flux on Flow in Curvilinear Diffusers
    
    TVT, 49:4 (2011),  557–567
17. The use of the hybrid RANS/ILES approach for the investigation of three-dimensional separated turbulent flows in curvilinear diffusers
    
    TVT, 48:2 (2010),  279–289
18. The application of hybrid RANS/ILES approach for the investigation of the effect of nozzle geometry and mode of efflux on the characteristics of turbulence of exhaust jets
    
    TVT, 47:3 (2009),  412–422
19. Development and applications of the efficient hybrid RANS/ILES approach for the calculation of complex turbulent jets
    
    TVT, 46:2 (2008),  271–282
20. The use of a one-parameter differential model of turbulence in numerical calculations with the aid of Navier–Stokes equations
    
    TVT, 36:1 (1998),  65–73
21. An efficient method for calculating the spatial flow around air intakes at transonic speeds
    
    Zh. Vychisl. Mat. Mat. Fiz., 31:9 (1991),  1355–1368
22. A modified method of approximate factorization when calculating three-dimensional potential flows in channels
    
    Zh. Vychisl. Mat. Mat. Fiz., 30:10 (1990),  1553–1570
23. Улучшение разрешения RANS/ILES(i)-методом турбулентных вихревых структур при дозвуковых числах Маха
    
    TVT, Forthcoming paper