Kirilovskiy Stanislav Viktorovich

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. Engineering modeling of a spatially inhomogeneous transition to turbulence on a swept wing
   
   Prikl. Mekh. Tekh. Fiz., 65:6 (2024),  147–151
4. Computational grids for engineering modeling of the laminar–turbulent flow
   
   Prikl. Mekh. Tekh. Fiz., 63:6 (2022),  91–95
5. 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
6. Determination of threshold $N$-factors of the laminar-turbulent transition in a subsonic boundary layer on a prolate spheroid
   
   Prikl. Mekh. Tekh. Fiz., 62:6 (2021),  3–7
7. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 62:2 (2021),  5–16
8. 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
9. Numerical study of the evolution of disturbances generated by roughness elements in a supersonic boundary layer on a blunted cone
   
   Prikl. Mekh. Tekh. Fiz., 60:3 (2019),  45–59
10. 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
11. Coefficients of transformation of long-wavelength perturbations of a supersonic incident flow around a wedge into pressure fluctuations on its surface
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:21 (2016),  70–78
12. A numerical study of non-equilibrium flows with different vibrational relaxation models
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 42:13 (2016),  72–79
13. Influence of vibrational relaxation on perturbations in a shock layer on a plate
    
    Zhurnal Tekhnicheskoi Fiziki, 85:5 (2015),  12–22
14. The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 41:4 (2015),  61–67
15. Engineering modeling of the laminar–turbulent transition: Achievements and problems (Review)
    
    Prikl. Mekh. Tekh. Fiz., 56:5 (2015),  30–49
16. Modeling of a supersonic flow around a cylinder with a gas-permeable porous insert
    
    Prikl. Mekh. Tekh. Fiz., 56:4 (2015),  12–22
17. ANSYS Fluent application for studying the influence of acoustic waves on a hypersonic shock layer over a flat plate
    
    Mat. Model., 25:9 (2013),  32–42
18. Control of disturbances of a hypersonic viscous shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 53:3 (2012),  38–47
19. 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