The purpose of the present paper is to report the numerical analysis of diffracting shock wave around a sharp-edged corner. The unsteady and nonviscous two-dimensional equations are solved with the piecewise liner method (PLM). The calculated results show that the diffracting shock waves around a corner have been classified into four types. Namely, they are normal, kink, Mach reflection and regular reflection types. The relation between the third shock wave and the vortex has been discussed. Furthermore, the calculated distribution of the pressure along a wall agrees with the experimental data, and the stagnation point on a wall has been observed
Geometrical Shock Dynamics (GSD) is a simplified model for nonlinear shock wave propagation for whic...
International audienceThe propagation of a planar shock wave through a split channel is both experim...
An explosion inside a cabin will converge at the corners to form high-pressure areas, significantly ...
The diffraction of a plane shock wave at a rounded corner was studied numerically. The numerical ana...
Lighthill's problem on the diffraction of shock wave past a convex corner has been investigated by t...
AbstractShock wave diffraction occurs when a normal travelling wave passes through a sudden area exp...
Results of numerical and analytical investigations of inviscid steady supersonic flows in corners fo...
The paper deals with the transition conditions from regular to irregular two-dimensional shock wave ...
As is well known when a shock wave is emitted from an open end of a tube, an expansion wave and a vo...
The production of vorticity or circulation production in shock wave diffraction over sharp convex co...
Studies of shock-vortex interactions in the past have predominantly been numerical, with a number of...
The unsteady reflection of cylindrical converging shock waves over convex obstacles is investigated ...
A separated oblique shock reflection on the floor of a rectangular cross-section wind tunnel has bee...
In the field of aerospace engineering, the study of the characteristics of vortical flows and their ...
In the field of aerospace engineering, the study of the characteristics of vortical flows and their ...
Geometrical Shock Dynamics (GSD) is a simplified model for nonlinear shock wave propagation for whic...
International audienceThe propagation of a planar shock wave through a split channel is both experim...
An explosion inside a cabin will converge at the corners to form high-pressure areas, significantly ...
The diffraction of a plane shock wave at a rounded corner was studied numerically. The numerical ana...
Lighthill's problem on the diffraction of shock wave past a convex corner has been investigated by t...
AbstractShock wave diffraction occurs when a normal travelling wave passes through a sudden area exp...
Results of numerical and analytical investigations of inviscid steady supersonic flows in corners fo...
The paper deals with the transition conditions from regular to irregular two-dimensional shock wave ...
As is well known when a shock wave is emitted from an open end of a tube, an expansion wave and a vo...
The production of vorticity or circulation production in shock wave diffraction over sharp convex co...
Studies of shock-vortex interactions in the past have predominantly been numerical, with a number of...
The unsteady reflection of cylindrical converging shock waves over convex obstacles is investigated ...
A separated oblique shock reflection on the floor of a rectangular cross-section wind tunnel has bee...
In the field of aerospace engineering, the study of the characteristics of vortical flows and their ...
In the field of aerospace engineering, the study of the characteristics of vortical flows and their ...
Geometrical Shock Dynamics (GSD) is a simplified model for nonlinear shock wave propagation for whic...
International audienceThe propagation of a planar shock wave through a split channel is both experim...
An explosion inside a cabin will converge at the corners to form high-pressure areas, significantly ...