Quasi-similar solution of the strong shock wave problem in non-ideal gas dynamics

2011 ◽  
Vol 337 (2) ◽  
pp. 597-604 ◽  
Author(s):  
L. P. Singh ◽  
S. D. Ram ◽  
D. B. Singh
Keyword(s):  
Shock Wave ◽  
Gas Dynamics ◽  
Strong Shock ◽  
Ideal Gas ◽  
Strong Shock Wave ◽  
Similar Solution ◽  
Wave Problem

scholarly journals An Exact Analytical Solution of the Strong Shock Wave Problem in Nonideal Magnetogasdynamics

2013 ◽  
Vol 2013 ◽  
pp. 1-4 ◽  
Author(s):  
S. D. Ram ◽  
R. Singh ◽  
L. P. Singh
Keyword(s):  
Magnetic Field ◽  
Shock Wave ◽  
Analytical Solution ◽  
Shock Front ◽  
Total Energy ◽  
Wave Motion ◽  
Exact Analytical Solution ◽  
Strong Shock ◽  
Strong Shock Wave ◽  
Wave Problem

We construct the solutions to the strong shock wave problem with generalized geometries in nonideal magnetogasdynamics. Here, it is assumed that the density ahead of the shock front varies according to a power of distance from the source of the disturbance. Also, an analytical expression for the total energy carried by the wave motion in nonideal medium under the influence of magnetic field is derived.

Sporadic interaction of a strong shock wave with a thin cone

1977 ◽  
Vol 11 (6) ◽  
pp. 919-924
Author(s):  
V. I. Bogatko ◽  
G. A. Kolton
Keyword(s):  
Shock Wave ◽  
Strong Shock ◽  
Strong Shock Wave

Axisymmetric hypersonic flow with strong viscous interaction

1968 ◽  
Vol 34 (4) ◽  
pp. 687-703 ◽  
Author(s):  
John Webster Ellinwood ◽  
Harold Mirels
Keyword(s):  
Shock Wave ◽  
Hypersonic Flow ◽  
Power Law ◽  
Axisymmetric Flow ◽  
Strong Shock ◽  
The Body ◽  
Strong Shock Wave ◽  
Viscous Interaction ◽  
Slender Bodies ◽  
Prandtl Numbers

Stewartson's theory for axisymmetric hypersonic flow of a model gas over slender bodies with strong viscous interaction and strong shock wave is extended to power-law viscosity variation and Prandtl numbers other than one. Flow properties at the body surface and shock are obtained without recourse to numerical integration. Numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong.

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