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Supersonic flows
Distribution of Mach number around a plate at M = 1.0
Visualization of Mechanical Processes
1669
Distribution of Mach number around a plate at M = 1.06
Visualization of Mechanical Processes
1749
Distribution of Mach number around a plate at M = 1.3
Visualization of Mechanical Processes
1765
Distribution of Mach number around a plate at M=1.82 and flow density 2.45∙10-4
Visualization of Mechanical Processes
1558
Distribution of Mach number around the diverged plate at M = 0.91
Visualization of Mechanical Processes
1726
Divergence of plate at M = 0.91
Visualization of Mechanical Processes
1654
Dynamics of the streaky structure at the initial stage of its breakdown
Visualization of Mechanical Processes
1637
Dynamics of the streaky structure at the late stage of its breakdown
Visualization of Mechanical Processes
1577
Evolution of the round parabolic jet in the cross flow in the xy plane
Visualization of Mechanical Processes
1816
Evolution of the round parabolic jet in the cross flow in the xz plane
Visualization of Mechanical Processes
1750
Evolution of the round parabolic jet in the cross flow in the xz plane; the acoustic frequency is 30 Hz
Visualization of Mechanical Processes
1620
Flow over a cavity during the continued variation of the cavity length
Visualization of Mechanical Processes
1750
Growth of the second natural mode of oscillations of a plate (M = 1.3)
Visualization of Mechanical Processes
1758
Instability of the streamwise vortex
Visualization of Mechanical Processes
1525
Perturbations of the streaky structure at the initial stage of its breakdown
Visualization of Mechanical Processes
1505
Perturbations of the streaky structure at the late stage of its breakdown
Visualization of Mechanical Processes
1711
Plate oscillation mode at M = 1.0 (corresponds to a borderline state between divergence and single mode flutter)
Visualization of Mechanical Processes
1602
Plate oscillations at M = 1.39 (the process is chaotic, with no specific mode dominated)
Visualization of Mechanical Processes
1555
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