Universal perturbation growth of Richtmyer–Meshkov instability for minimum-surface featured interface induced by weak shock waves

2021 ◽  
Vol 33 (3) ◽  
pp. 032110
Author(s):  
Yu Liang ◽  
Lili Liu ◽  
Zhigang Zhai ◽  
Ting Si ◽  
Xisheng Luo
Keyword(s):  
Shock Waves ◽  
Weak Shock ◽  
Minimum Surface ◽  
Perturbation Growth

Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge

2020 ◽  
Author(s):  
V. L. Kocharin ◽  
A. A. Yatskikh ◽  
D. S. Prishchepova ◽  
A. V. Panina ◽  
Yu. G. Yermolaev ◽  
...  
Keyword(s):  
Heat Transfer ◽  
Boundary Layer ◽  
Experimental Study ◽  
Shock Waves ◽  
Flat Plate ◽  
Leading Edge ◽  
Weak Shock ◽  
The Impact

Effects of Viscosity on Steady Reflection of Weak Shock Waves

2008 ◽  
Author(s):  
Mikhail Ivanov ◽  
Yevgeny Bondar ◽  
Dmitry Khotyanovsky ◽  
Alexey Kudryavtsev ◽  
Georgiy Shoev
Keyword(s):  
Shock Waves ◽  
Weak Shock

On the propagation of weak shock waves in compressible thermohyperelastic solids

2017 ◽  
Vol 229 (1) ◽  
pp. 87-97 ◽  
Author(s):  
Hocine Bechir ◽  
Abdelhakim Benslimane
Keyword(s):  
Shock Waves ◽  
Weak Shock

On nonlinear diffraction of weak shock waves

1971 ◽  
Vol 35 (3) ◽  
pp. 447-452
Author(s):  
L.I. Mogilevich ◽  
G.P. Shindiapin
Keyword(s):  
Shock Waves ◽  
Weak Shock ◽  
Nonlinear Diffraction

Effect of weak shock waves on diamond powders and compacted modifications of boron nitride

1991 ◽  
Vol 30 (7) ◽  
pp. 599-603
Author(s):  
V. I. Kovtun ◽  
V. F. Britun ◽  
V. I. Trefilov ◽  
A. N. Pilyankevich ◽  
M. V. Karpets
Keyword(s):  
Boron Nitride ◽  
Shock Waves ◽  
Weak Shock ◽  
Diamond Powders

Numerical Analysis of the Oblique Reflection of Weak Shock Waves

1995 ◽  
pp. 187-190
Author(s):  
M. Itabashi ◽  
H. Honma ◽  
N. Watanabe ◽  
S. Harada
Keyword(s):  
Numerical Analysis ◽  
Shock Waves ◽  
Weak Shock ◽  
Oblique Reflection

scholarly journals Experimental study of weak shock waves influence on the supersonic boundary layer of the flat plate model

2019 ◽  
Vol 196 ◽  
pp. 00018 ◽  
Author(s):  
Vasiliy Kocharin ◽  
Aleksandr Kosinov ◽  
Yuriy Yermolayev ◽  
Nikolay Semionov
Keyword(s):  
Boundary Layer ◽  
Experimental Study ◽  
Shock Waves ◽  
Flat Plate ◽  
Leading Edge ◽  
Weak Shock ◽  
Supersonic Boundary Layer ◽  
Complex Flow ◽  
Complex Flow Structure ◽  
Constant Temperature Anemometer

The experimental study of the effect of weak shock waves on the supersonic boundary layer of the flat plate with a blunt leading edge (the radius of bluntness was r = 2.5 mm) with Mach number M = 2.5 and zero angle of attack was carried out. The measurements were carried out using the constant temperature anemometer. The paper presents a complex flow structure on the surface of the model. High-intensity peaks were found in the regions of the disturbed flow. Also the spectral analysis of perturbations was performed. It is found that the supersonic boundary layer on a flat plate is very sensitive to the effect of weak shock waves.

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