Shur Mikhail L'vovich

Publications in Math-Net.Ru

1. Numerical simulation of evolution of a curved turbulent wake subjected to adverse pressure gradient
   
   Mat. Model., 35:10 (2023),  3–18
2. Two-stage RANS-DDES model and results of computations of unsteady loads on reentry capsule and engine compartment of manned spacecraft in the course of their emergency separation
   
   Mat. Model., 33:7 (2021),  121–138
3. Simulation of impact of the wakes of emergency rescue unit’s nozzles on the surface of a manned spacecraft
   
   Mat. Model., 33:7 (2021),  18–34
4. Les-based computation of evolution of turbulent wakes subjected to adverse pressure gradient
   
   Mat. Model., 32:6 (2020),  3–20
5. Flow and noise prediction for tandem cylinder
   
   Mat. Model., 26:6 (2014),  119–136
6. LES-based evaluation of a micro-jet noise reduction concept in static and flight conditions
   
   Mat. Model., 23:11 (2011),  48–64
7. Numerical prediction of jet-noise based on “first principles”
   
   Mat. Model., 19:7 (2007),  5–26
8. Numerical modeling of separation control by mechanical and jet vortex generators
   
   Mat. Model., 18:3 (2006),  55–68
9. Analysis of three-dimensional turbulent flow in an $S$-shaped rectangular channel
   
   TVT, 41:1 (2003),  57–64
10. The calculation of $\mathrm{HF}$ chemical lasers in view of interference between the processes in the combustion zone and in nozzle unit
    
    TVT, 37:4 (1999),  647–655
11. Numerical modelling of a supersonic cw chemical HF laser with a three-jet nozzle array
    
    Kvantovaya Elektronika, 25:5 (1998),  387–391
12. Assessment of applicability of modern models of turbulence for calculation of natural-convection flows and heat transfer
    
    TVT, 36:2 (1998),  246–254
13. A comparison between one- and two-equation differential models of turbulence in application to separated and attached flows: Transonic flows around airfoil
    
    TVT, 35:2 (1997),  301–313
14. A comparison of the capabilities of one- and two-equation differential models of turbulence in application to separated and attached flows in a channel with forward-facing step
    
    TVT, 34:6 (1996),  896–902
15. A comparison between one- and two-equation differential turbulence models in application to separated and attached flows: Flow in channel with counterstep
    
    TVT, 34:5 (1996),  724–736
16. The calculation of steady turbulent flows of chemically reacting gGas mixtures in channels at arbitrary Mach numbers
    
    TVT, 32:6 (1994),  850–862
17. Calculation of steady-state three-dimensional flows of viscous gas in channels and nozzles
    
    TVT, 31:3 (1993),  395–405
18. Influence of three-dimensional effects on fluid dynamics and heat transfer in the subsonic flow of a viscous compressible gas on the initial section of a rectangular channel
    
    TVT, 29:5 (1991),  967–972
19. Calculation of steady-state three-dimensional flows of viscous gases and chemically reacting gas mixtures
    
    Zh. Vychisl. Mat. Mat. Fiz., 31:2 (1991),  300–316
20. Application of compressibility scaling method for calculation of steady viscous gas and gas mixture flows in Laval nozzles
    
    Mat. Model., 2:10 (1990),  3–12
21. Subsonic compressible flows of chemically reacting gas mixtures in cylindrical and rectangular channels with sudden expansion
    
    TVT, 28:6 (1990),  1149–1155
22. Influence of compressibility of the hydrodynamics and heat-transfer in subsonic viscous-gas flows in channels in the presence of recirculation zones
    
    TVT, 27:2 (1989),  292–299
23. Methods of scaling the compressibility in calculating stationary flows of a viscous gas at arbitrary Mach numbers
    
    Zh. Vychisl. Mat. Mat. Fiz., 28:2 (1988),  254–266
24. Numerical analysis of operating conditions of a continuous-action HF chemical laser
    
    Fizika Goreniya i Vzryva, 15:1 (1979),  89–97