Tsyryulnikov Ivan Sergeevich

Publications in Math-Net.Ru

1. 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
2. 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
3. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow
   
   Prikl. Mekh. Tekh. Fiz., 62:2 (2021),  5–16
4. 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
5. 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
6. ANSYS Fluent application for studying the influence of acoustic waves on a hypersonic shock layer over a flat plate
   
   Matem. Mod., 25:9 (2013),  32–42
7. 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
8. Control of disturbances of a hypersonic viscous shock layer on a flat plate
   
   Prikl. Mekh. Tekh. Fiz., 53:3 (2012),  38–47
9. 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
10. Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers
    
    Prikl. Mekh. Tekh. Fiz., 53:1 (2012),  3–11
11. Wave processes in the shock layer on a flat plate at an angle of attack
    
    Prikl. Mekh. Tekh. Fiz., 51:4 (2010),  39–47
12. Effect of streamwise structures on heat transfer in a hypersonic flow in a compression corner
    
    Prikl. Mekh. Tekh. Fiz., 50:4 (2009),  112–120
13. Numerical simulation of receptivity of a hypersonic boundary layer to acoustic disturbances
    
    Prikl. Mekh. Tekh. Fiz., 48:3 (2007),  84–91
14. 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