Boundary-layer transition from a laminar to a turbulent regime is a critical driver in the design of high-speed vehicles. The aerothermodynamic loads associated with transitional or fully turbulent hypersonic boundary layers are several times higher than those associated with laminar flow. The presence of isolated roughness elements on the surface of a body can accelerate the growth of incoming disturbances and introduce additional instability mechanisms in the flow field, eventually leading to a premature occurrence of transition. This dissertation studies the instabilities induced by three-dimensional discrete roughness elements located inside a high-speed boundary layer developing on a flat plate. Two-dimensional local linear stability t...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Boundary layer transition is a relevant phenomenon in many aerodynamic and aero-thermodynamic proble...
The linear instability and breakdown to turbulence induced by an isolated roughness element in a bou...
The linear instability and breakdown to turbulence induced by an isolated roughnesselement in a boun...
The linear instability and breakdown to turbulence induced by an isolated roughness element in a bou...
The current understanding and research efforts on surface roughness effects in hypersonic boundary-l...
The influence of high-temperature effects on the stability of the wake behind a cuboidal roughness e...
In this work the effect of isolated surface roughness on the behaviour of a hypersonic boundary laye...
The linear global instability and resulting transition to turbulence induced by anisolated cylindric...
The excitation of instability modes in the wake generated behind a discrete roughness element in a b...
Progress on a joint experimental and numerical study of laminar-to-turbulent transition induced by a...
The linear global instability and resulting transition to turbulence induced by an isolated cylindri...
A deeper understanding of the different factors that influence the laminar-turbulent transition in s...
Surface roughness is known to have a substantial impact on the aerothermodynamic loading of high-spe...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Boundary layer transition is a relevant phenomenon in many aerodynamic and aero-thermodynamic proble...
The linear instability and breakdown to turbulence induced by an isolated roughness element in a bou...
The linear instability and breakdown to turbulence induced by an isolated roughnesselement in a boun...
The linear instability and breakdown to turbulence induced by an isolated roughness element in a bou...
The current understanding and research efforts on surface roughness effects in hypersonic boundary-l...
The influence of high-temperature effects on the stability of the wake behind a cuboidal roughness e...
In this work the effect of isolated surface roughness on the behaviour of a hypersonic boundary laye...
The linear global instability and resulting transition to turbulence induced by anisolated cylindric...
The excitation of instability modes in the wake generated behind a discrete roughness element in a b...
Progress on a joint experimental and numerical study of laminar-to-turbulent transition induced by a...
The linear global instability and resulting transition to turbulence induced by an isolated cylindri...
A deeper understanding of the different factors that influence the laminar-turbulent transition in s...
Surface roughness is known to have a substantial impact on the aerothermodynamic loading of high-spe...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Compared to laminar flow, turbulent flow causes significantly higher drag and heat transfer to an ob...
Boundary layer transition is a relevant phenomenon in many aerodynamic and aero-thermodynamic proble...