The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional disturbances of a uniform, supersonic, freestream flow are investigated. The paper extends the two-dimensional study of Duck et alx, through the use of vector potentials, which render the problem tractable by the same techniques as in the two-dimensional case, in particular by expansion of the solution by means of a Fourier-Bessel series, in appropriately chosen coordinates. Results are presented for specific classes of freestream disturbances, and the study shows conclusively that the shock is stable to all classes of disturbances (i.e. time periodic per-turbations to the shock do not grow downstream), provided the flow downstream of the shock...
The supersonic biplane is well known for the airfoil which has zero wave drag at the supersonic spee...
When a plane shock hits a wedge head on, it experiences a reflection and then a self-similar reflect...
It is well known that, when the vertex angle of a straight wedge is less than the critical angle, th...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
When an upstream steady uniform supersonic flow impinges onto a symmetric straight-sided wedge, gove...
AbstractAs is well known, two solutions of the problem of a supersonic stationary inviscid nonheatco...
In this paper, we are concerned with the instability problem of a 3-D transonic oblique shock wave f...
AbstractIn this paper we study the stability of transonic shocks in steady supersonic flow past a we...
A theoretical investigation of the breakdown of the viscous wake downstream of a flat plate in super...
This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supe...
In this paper the work of Lighthill (1) for one-diniensional unsteady motion is extended to the prob...
We are studying the problem of a stationary supersonic flow of an inviscid non-heat-conducting gas i...
The response of asymmetric and planar shock interactions to a continuous excitation of the lower inc...
AbstractWhen a wing with a sharp leading edge is placed in a supersonic flow with a small attack ang...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
The supersonic biplane is well known for the airfoil which has zero wave drag at the supersonic spee...
When a plane shock hits a wedge head on, it experiences a reflection and then a self-similar reflect...
It is well known that, when the vertex angle of a straight wedge is less than the critical angle, th...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
When an upstream steady uniform supersonic flow impinges onto a symmetric straight-sided wedge, gove...
AbstractAs is well known, two solutions of the problem of a supersonic stationary inviscid nonheatco...
In this paper, we are concerned with the instability problem of a 3-D transonic oblique shock wave f...
AbstractIn this paper we study the stability of transonic shocks in steady supersonic flow past a we...
A theoretical investigation of the breakdown of the viscous wake downstream of a flat plate in super...
This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supe...
In this paper the work of Lighthill (1) for one-diniensional unsteady motion is extended to the prob...
We are studying the problem of a stationary supersonic flow of an inviscid non-heat-conducting gas i...
The response of asymmetric and planar shock interactions to a continuous excitation of the lower inc...
AbstractWhen a wing with a sharp leading edge is placed in a supersonic flow with a small attack ang...
An analytical investigation is performed to study the unsteady response of a one-dimensional, non-li...
The supersonic biplane is well known for the airfoil which has zero wave drag at the supersonic spee...
When a plane shock hits a wedge head on, it experiences a reflection and then a self-similar reflect...
It is well known that, when the vertex angle of a straight wedge is less than the critical angle, th...