Direct numerical simulations are carried out on boundary-layer flow at Mach 6 over a porous surface, in which a Mack mode of instability is excited. The pores are resolved rather than modeled, allowing an evaluation to be made of the accuracy of simplified analytical models used in previous investigations based on linear stability theory. It is shown that the stabilizing effect of porosity is stronger in the simulations than in the corresponding theory for both two- and three-dimensional pores. From comparisons of spanwise grooves, streamwise slots, and square pores, it appears that the detailed surface structure is not as important as the overall porosity, and the hydraulic diameter is able to collapse the results for different pore shapes...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...
The present numerical investigation of the effect of porous surfaces on transition in hypersonic bou...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface...
Transition to turbulence of a Mach 6 flat plate boundary layer over a porous surface is investigated...
The flow field over a 3 degree blunt cone is investigated with respect to a hypersonic stability ana...
The flow field over a 3 degree blunt cone is investigated with respect to a hypersonic stability ana...
The acoustic second-mode instability predicted by linear stability theory is compared with direct nu...
The effect of porous coating on the instability of a Mach 5.92 flat-plate boundary layer is investig...
The flow field over a 3° blunt cone is investigated with respect to a hypersonic stability analysis ...
Hypersonic laminar flow control for delayed laminar-turbulent transition is of high importance for r...
The flow field over a 3° blunt cone is investigated with respect to a hypersonic stability analysis ...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...
The present numerical investigation of the effect of porous surfaces on transition in hypersonic bou...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface,...
Direct numerical simulations are carried out of boundary layer flow at Mach 6 over a porous surface...
Transition to turbulence of a Mach 6 flat plate boundary layer over a porous surface is investigated...
The flow field over a 3 degree blunt cone is investigated with respect to a hypersonic stability ana...
The flow field over a 3 degree blunt cone is investigated with respect to a hypersonic stability ana...
The acoustic second-mode instability predicted by linear stability theory is compared with direct nu...
The effect of porous coating on the instability of a Mach 5.92 flat-plate boundary layer is investig...
The flow field over a 3° blunt cone is investigated with respect to a hypersonic stability analysis ...
Hypersonic laminar flow control for delayed laminar-turbulent transition is of high importance for r...
The flow field over a 3° blunt cone is investigated with respect to a hypersonic stability analysis ...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...
The present numerical investigation of the effect of porous surfaces on transition in hypersonic bou...
The damping of acoustic second mode instabilities by passive porous surfaces is investigated numeric...