We examine the interaction of shock waves by studying solutions of the two-dimensional Euler equations about a point. The problem is reduced to linear form by considering local solutions that are constant along each ray and thereby exhibit no length scale at the intersection point. Closed-form solutions are obtained in a unified manner for standard gasdynamics problems including oblique shock waves, Prandtl– Meyer flow and Mach reflection. These canonical gas dynamical problems are shown to reduce to a series of geometrical transformations involving anisotropic coordinate stretching and rotation operations. An entropy condition and a requirement for geometric regularity of the intersection of the incident waves are used to eliminate spuriou...
This paper is the continuation of [LiJ]. We take into account the existence of global continuous sol...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...
We examine the interaction of shock waves by studying solutions of the two-dimensional Euler equatio...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
AbstractEnhanced resolution for the computation of the interaction of shock waves with fluid interfa...
We are concerned with the Riemann problem for the two-dimensional compressible Euler equations in ga...
Abstract. We consider the problem of resolving all pairwise interactions of shock waves, con-tact wa...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
This paper is the continuation of [LiJ]. We take into account the existence of global continuous sol...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...
We examine the interaction of shock waves by studying solutions of the two-dimensional Euler equatio...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
The main objective of this dissertation is to detect and study the phenomena of reflection of one sh...
AbstractEnhanced resolution for the computation of the interaction of shock waves with fluid interfa...
We are concerned with the Riemann problem for the two-dimensional compressible Euler equations in ga...
Abstract. We consider the problem of resolving all pairwise interactions of shock waves, con-tact wa...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
The morphology of nodes generated by the interaction of discontinuities in steady two-dimensional in...
This paper is the continuation of [LiJ]. We take into account the existence of global continuous sol...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...
The impingement of shock waves on blunt bodies in steady supersonic flow is known to cause extremely...