Mironov Sergei Grigor'evich

Publications in Math-Net.Ru

1. Shock wave reflection from highly porous barriers with inhomogeneous structures
   
   Prikl. Mekh. Tekh. Fiz., 66:5 (2025),  105–116
2. Interaction of shock waves with gas-permeable cellular-porous materials
   
   Prikl. Mekh. Tekh. Fiz., 66:2 (2025),  17–28
3. Effect of the jet pressure ratio in supersonic axisymmetric jets of a polyatomic gas SF$_6$ on their gas-dynamic structure
   
   Prikl. Mekh. Tekh. Fiz., 65:1 (2024),  47–57
4. Similarity parameter for the drag coefficient of a cylinder with a high-porosity frontal insert aligned at an angle of attack in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 63:6 (2022),  82–90
5. Controlling the aerodynamic drag of a cylinder with gas-permeable porous inserts by regulating base pressure
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 47:8 (2021),  41–43
6. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 62:2 (2021),  5–16
7. Physical and mathematical modeling of a supersonic flow around bodies with gas-permeable porous inserts at an angle of attack
   
   Prikl. Mekh. Tekh. Fiz., 61:5 (2020),  14–20
8. A similarity criterion for supersonic flow past a cylinder with a frontal high-porosity cellular insert
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 44:6 (2018),  3–10
9. An experimental study of the structure of supersonic flat underexpanded microjets
   
   Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:10 (2015),  97–103
10. The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:4 (2015),  61–67
11. Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert
    
    Prikl. Mekh. Tekh. Fiz., 56:4 (2015),  12–22
12. Controlling aerodynamic forces with the aid of gas-permeable porous materials
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 40:19 (2014),  83–88
13. Relaminarization in supersonic microjets at low Reynolds numbers
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 39:16 (2013),  47–54
14. Stability of a subsonic gas microjet
    
    Zhurnal Tekhnicheskoi Fiziki, 82:2 (2012),  17–23
15. Effect of sound-absorbing materials on intensity of disturbances in the shock layer on a flat plate aligned at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 53:2 (2012),  21–32
16. Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers
    
    Prikl. Mekh. Tekh. Fiz., 53:1 (2012),  3–11
17. Effect of nozzle size on supersonic microjet length
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 37:22 (2011),  10–15
18. Physical and mathematical modeling of a supersonic flow around a cylinder with a porous insert
    
    Prikl. Mekh. Tekh. Fiz., 52:1 (2011),  13–23
19. Wave processes in the shock layer on a flat plate at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 51:4 (2010),  39–47
20. Effect of streamwise structures on heat transfer in a hypersonic flow in a compression corner
    
    Prikl. Mekh. Tekh. Fiz., 50:4 (2009),  112–120
21. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances
    
    Prikl. Mekh. Tekh. Fiz., 48:3 (2007),  84–91
22. Optical study of vibrational combustion of hydrogen in tubes
    
    Fizika Goreniya i Vzryva, 42:1 (2006),  34–38
23. Experimental study and direct numerical simulation of the evolution of disturbances in a viscous shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 47:5 (2006),  3–15
24. Evolution of controlled disturbances in the shock layer on the compression surface
    
    Prikl. Mekh. Tekh. Fiz., 44:5 (2003),  30–38
25. Experimental study of stability of strongly underexpanded laminar free and impact jets
    
    Prikl. Mekh. Tekh. Fiz., 42:6 (2001),  39–46
26. Numerical simulation of hypersonic flow around a sharp cone
    
    Prikl. Mekh. Tekh. Fiz., 42:3 (2001),  43–50
27. Experimental study of density fluctuations in a hypersonic laminar wake behind a cone
    
    Prikl. Mekh. Tekh. Fiz., 41:3 (2000),  111–117
28. Experimental study of vortex structures in a hypersonic shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 40:6 (1999),  41–47
29. Investigation of aerodynamic heating of a plate in a viscous hypersonic flow
    
    TVT, 37:3 (1999),  415–419
30. The effect of the angle of attack on hypersonic flow on a plate
    
    TVT, 36:5 (1998),  754–760
31. An experimental study of density fluctuations in the hypersonic boundary layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 37:6 (1996),  51–60
32. Hypersonic flow on a flat plate. Experimental results and numerical modeling
    
    Prikl. Mekh. Tekh. Fiz., 36:6 (1995),  60–67
33. Spectral composition of wave numbers of longitudinal vortices and characteristics of flow structure in a supersonic jet
    
    Prikl. Mekh. Tekh. Fiz., 34:5 (1993),  41–47
34. Influence of the outer feedback loop parameters on the free oscillations of the flow of an underexpanded jet past a finite obstacle
    
    Prikl. Mekh. Tekh. Fiz., 34:1 (1993),  94–100
35. Oscillations in the parallel discharge of two supersonic nonisobaric jets
    
    Prikl. Mekh. Tekh. Fiz., 33:5 (1992),  29–36
36. Features of separated supersonic flow pulsations ahead of a spike-tipped cylinder
    
    Prikl. Mekh. Tekh. Fiz., 32:6 (1991),  101–108
37. Experimental study of pulsations in the forward separation zone in a supersonic flow
    
    Prikl. Mekh. Tekh. Fiz., 30:4 (1989),  116–124
38. Scattering of 0.15–1.8-eV argon atoms from a germanium surface
    
    Prikl. Mekh. Tekh. Fiz., 17:4 (1976),  157–163
39. Use of excited atoms to study the Ar component in a molecular beam obtained from an Ar–He mixture
    
    Prikl. Mekh. Tekh. Fiz., 16:4 (1975),  45–51