Tsyryulnikov Ivan Sergeevich

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. Numerical simulation of the flow in a sensor for measuring the flow stagnation temperature in pulsed aerodynamic installations
   
   Prikl. Mekh. Tekh. Fiz., 63:3 (2022),  75–87
5. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 62:2 (2021),  5–16
6. 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
7. 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
8. Influence of vibrational relaxation on perturbations in a shock layer on a plate
   
   Zhurnal Tekhnicheskoi Fiziki, 85:5 (2015),  12–22
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. Controlling aerodynamic forces with the aid of gas-permeable porous materials
    
    Pisma v Zhurnal Tekhnicheskoi Fiziki, 40:19 (2014),  83–88
12. 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
13. Stability of a subsonic gas microjet
    
    Zhurnal Tekhnicheskoi Fiziki, 82:2 (2012),  17–23
14. Experimental verification of the method of calculating the flow parameters in the test section of the hotshot wind tunnel
    
    Prikl. Mekh. Tekh. Fiz., 53:5 (2012),  79–89
15. Control of disturbances of a hypersonic viscous shock layer on a flat plate
    
    Prikl. Mekh. Tekh. Fiz., 53:3 (2012),  38–47
16. 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
17. Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers
    
    Prikl. Mekh. Tekh. Fiz., 53:1 (2012),  3–11
18. Wave processes in the shock layer on a flat plate at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 51:4 (2010),  39–47
19. Effect of streamwise structures on heat transfer in a hypersonic flow in a compression corner
    
    Prikl. Mekh. Tekh. Fiz., 50:4 (2009),  112–120
20. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances
    
    Prikl. Mekh. Tekh. Fiz., 48:3 (2007),  84–91
21. 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