The transition process which takes place in the attachment-line boundary layer in the presence of gross contamination is an issue of considerable interest to wing designers. It is well known that this flow is very sensitive to the presence of isolated roughness and that transition can be initiated at a very low value of the local medium thickness Reynolds number.Moreover, once the attachment line is turbulent, the flow over the whole wing chords, top and bottom surface, will be turbulent and this has major implications for wind drag
This investigation shows that the properties of the two-dimensional flow around a high-lift multi-el...
The emphasis in this work is on the effects of the propeller slipstream on the behavior of boundary ...
The transition from laminar to turbulent flow in a boundary layer is a complex phenomenon that may t...
Due to a singularity in the governing three-dimensional turbulent momentum integral equations at the...
Flight tests on the Handley Page suction wing showed that turbulence, generated at the wing root, c...
On a swept wing, contamination along the leading edge, Tollmien-Schlichting waves, stationary or tra...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
Recent experimental studies of laminar-turbulent transition are presented withfocus on adverse press...
One of the possible forcing mechanisms for inducing transition from laminar to turbulent flow is fre...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
An experimental study was carried out to understand the way the turbulence interacts with the bounda...
The instability of an infinite swept attachment line boundary layer is considered in the linear regi...
AbstractThe large-eddy simulation (LES) technique is applied to the subcritical transition to turbul...
Transition to turbulence in boundary layer flows is a process involving several steps: receptivity t...
Transition to turbulence in swept-wing flows has resisted correlation with linear theory because of ...
This investigation shows that the properties of the two-dimensional flow around a high-lift multi-el...
The emphasis in this work is on the effects of the propeller slipstream on the behavior of boundary ...
The transition from laminar to turbulent flow in a boundary layer is a complex phenomenon that may t...
Due to a singularity in the governing three-dimensional turbulent momentum integral equations at the...
Flight tests on the Handley Page suction wing showed that turbulence, generated at the wing root, c...
On a swept wing, contamination along the leading edge, Tollmien-Schlichting waves, stationary or tra...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
Recent experimental studies of laminar-turbulent transition are presented withfocus on adverse press...
One of the possible forcing mechanisms for inducing transition from laminar to turbulent flow is fre...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
An experimental study was carried out to understand the way the turbulence interacts with the bounda...
The instability of an infinite swept attachment line boundary layer is considered in the linear regi...
AbstractThe large-eddy simulation (LES) technique is applied to the subcritical transition to turbul...
Transition to turbulence in boundary layer flows is a process involving several steps: receptivity t...
Transition to turbulence in swept-wing flows has resisted correlation with linear theory because of ...
This investigation shows that the properties of the two-dimensional flow around a high-lift multi-el...
The emphasis in this work is on the effects of the propeller slipstream on the behavior of boundary ...
The transition from laminar to turbulent flow in a boundary layer is a complex phenomenon that may t...