The nonlinear stability of a compressible flow past a wedge is investigated in the hypersonic limit. The analysis follows the ideas of a weakly nonlinear approach. Interest is focussed on Tollmien-Schlichting waves governed by a triple deck structure and it is found that the attached shock can profoundly affect the stability characteristics of the flow. In particular, it is shown that nonlinearity tends to have a stabilizing influence. The nonlinear evolution of the Tollmien-Schlichting mode is described in a number of asymptotic limits
AbstractA nonlinear stability analysis using a multiple-scales perturbation procedure is performed f...
When an upstream steady uniform supersonic flow impinges onto a symmetric straight-sided wedge, gove...
Leading-edge receptivity to fast and slow acoustic waves of boundary layers on a cylinder���wedge ge...
The instability of a compressible flow past a wedge is investigated in the hypersonic limit. Particu...
In this paper an oscillating wedge has been considered, and the fluid slabs are kept at 900 to the w...
The instability of hypersonic boundary-layer flows over flat plates is considered. The viscosity of ...
Several aspects of the oscillating wedge are investigated to evaluate both the resulting trends for ...
AbstractIn this paper we study the stability of transonic shocks in steady supersonic flow past a we...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
The self-excited spanwise homogeneous perturbations arising in shock-wave/boundary-layer interaction...
In this paper, the shock pattern oscillations induced by shock/shock interactions over double-wedge ...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
A systematic study is made of the approximate inviscid theory of thin bodies moving at such high sup...
We consider the problem of two-dimensional supersonic flow onto a solid wedge, or equivalently in a ...
In this paper, we are concerned with the instability problem of a 3-D transonic oblique shock wave f...
AbstractA nonlinear stability analysis using a multiple-scales perturbation procedure is performed f...
When an upstream steady uniform supersonic flow impinges onto a symmetric straight-sided wedge, gove...
Leading-edge receptivity to fast and slow acoustic waves of boundary layers on a cylinder���wedge ge...
The instability of a compressible flow past a wedge is investigated in the hypersonic limit. Particu...
In this paper an oscillating wedge has been considered, and the fluid slabs are kept at 900 to the w...
The instability of hypersonic boundary-layer flows over flat plates is considered. The viscosity of ...
Several aspects of the oscillating wedge are investigated to evaluate both the resulting trends for ...
AbstractIn this paper we study the stability of transonic shocks in steady supersonic flow past a we...
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional di...
The self-excited spanwise homogeneous perturbations arising in shock-wave/boundary-layer interaction...
In this paper, the shock pattern oscillations induced by shock/shock interactions over double-wedge ...
The development of the flow pattern that arises during the interaction of a shock wave with a wedge ...
A systematic study is made of the approximate inviscid theory of thin bodies moving at such high sup...
We consider the problem of two-dimensional supersonic flow onto a solid wedge, or equivalently in a ...
In this paper, we are concerned with the instability problem of a 3-D transonic oblique shock wave f...
AbstractA nonlinear stability analysis using a multiple-scales perturbation procedure is performed f...
When an upstream steady uniform supersonic flow impinges onto a symmetric straight-sided wedge, gove...
Leading-edge receptivity to fast and slow acoustic waves of boundary layers on a cylinder���wedge ge...