Numerical Study of a Turbulent Flow Compressed by a Weak Shock Wave

1997 ◽  
Vol 8 (1) ◽  
pp. 63-75 ◽  
Author(s):  
T. HASEGAWA ◽  
S. NOGUCHI
Shock Waves ◽  
1996 ◽  
Vol 6 (5) ◽  
pp. 287-300 ◽  
Author(s):  
P. Mazel ◽  
R. Saurel ◽  
J. -C. Loraud ◽  
P. B. Butler

Shock Waves ◽  
1996 ◽  
Vol 6 (5) ◽  
pp. 287-300 ◽  
Author(s):  
P. Mazel ◽  
R. Saurel ◽  
J.-C. Loraud ◽  
P.B. Butler

Shock Waves ◽  
2018 ◽  
Vol 29 (2) ◽  
pp. 273-284 ◽  
Author(s):  
W. Zhang ◽  
L. Zou ◽  
X. Zheng ◽  
B. Wang

2010 ◽  
Vol 22 (6) ◽  
pp. 061703 ◽  
Author(s):  
J. Giordano ◽  
J. D. Parisse ◽  
L. Biamino ◽  
J. Devesvre ◽  
P. Perrier

Author(s):  
Jean-Franc¸ois Sigrist

The present paper exposes an analytical and numerical study of the interaction between a weak shock wave and an immersed elastic structure. Several models of the problem are exposed and compared in the study: on the one hand, a semi-analytical method is proposed and on the other hand a numerical method is developed, based on a description of fluid-structure interaction through i) exact and ii) simplified interaction models. Comparison of the various approaches is exposed on a simple analytical case, namely that of a two-dimensional circular shell immersed in a two-dimensional compressible fluid and subjected to a spherical shock wave. Discussion of the various numerical results gives some practical guidance for the use of simplified fluid-structure interaction models in the context of industrial studies for underwater shock analysis.


2019 ◽  
Vol 160 ◽  
pp. 552-557 ◽  
Author(s):  
Rahul Kumar Chaturvedi ◽  
Pooja Gupta ◽  
L.P. Singh

2005 ◽  
Vol 542 (-1) ◽  
pp. 105 ◽  
Author(s):  
BERIC W. SKEWS ◽  
JASON T. ASHWORTH

Author(s):  
K. Stewartson

AbstractThe effect on the boundary-layer equations of a weak shock wave of strength ∈ has been investigated, and it is shown that ifRis the Reynolds number of the boundary layer, separation occurs when ∈ =o(R−i). The boundary-layer assumptions are then investigated and shown to be consistent. It is inferred that separation will occur if a shock wave meets a boundary and the above condition is satisfied.


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