Results are reported from an extensive series of experiments on boundary layers in which the location of pressure gradient and transition onset could be varied almost independently, by judicious use of tunnel wall liners and transition-fixing devices. The experiments show that the transition zone is sensitive to the pressure gradient especially near onset, and can be significantly asymmetric; no universal similarity appears valid in general. Observed intermittency distributions cannot be explained on the basis of the hypothesis, often made, that the spot propagates at speeds proportional to the local free-stream velocity but is otherwise unaffected by the pressure gradient
Transition in the boundary layer on a flat plate is examined from the point of view of intermittent ...
The effect of lateral streamline convergence alone on the transitional flow characteristics has been...
Boundary layer transition was measured in zero, favorable, and adverse pressure gradients at Mach 8 ...
Results are reported from an extensive series of experiments on boundary layers in which the locatio...
This paper is a survey of certain recent advances in our understanding of the transition zone in a b...
The calculation of the transitional boundary layer requires estimates of the extent of the transitio...
This paper is a survey of certain recent advances in our understanding of the transition zone in a b...
The flow during transition from the laminar to a turbulent state in a boundary layer is best describ...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
The method proposed here considers the mean flow in the transition zone as a linear combination of t...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
The influence of the streamwise pressure gradient and a nonadiabatic surface on boundary layer trans...
High velocity boundary layer transition experiments are performed in a Ludwieg tube set-up. At a Mac...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
Transition in the boundary layer on a flat plate is examined from the point of view of intermittent ...
The effect of lateral streamline convergence alone on the transitional flow characteristics has been...
Boundary layer transition was measured in zero, favorable, and adverse pressure gradients at Mach 8 ...
Results are reported from an extensive series of experiments on boundary layers in which the locatio...
This paper is a survey of certain recent advances in our understanding of the transition zone in a b...
The calculation of the transitional boundary layer requires estimates of the extent of the transitio...
This paper is a survey of certain recent advances in our understanding of the transition zone in a b...
The flow during transition from the laminar to a turbulent state in a boundary layer is best describ...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
The method proposed here considers the mean flow in the transition zone as a linear combination of t...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
The influence of the streamwise pressure gradient and a nonadiabatic surface on boundary layer trans...
High velocity boundary layer transition experiments are performed in a Ludwieg tube set-up. At a Mac...
Recent developments in the modelling of the transition zone in the boundary layer are reviewed (the ...
Transition in the boundary layer on a flat plate is examined from the point of view of intermittent ...
The effect of lateral streamline convergence alone on the transitional flow characteristics has been...
Boundary layer transition was measured in zero, favorable, and adverse pressure gradients at Mach 8 ...