The temporal stability characteristics of generic, swept-wing boundary-layer flows of practical engineering significance with a smooth, isolated backward facing step or a forward-facing step are investigated. A streamwise BiGlobal analysis is undertaken on previously computed steady-state, Mach 0.3 Navier-Stokes solutions that had been obtained for four spanwise invariant step heights and at two chordwise locations on an infinite swept-wing geometry. Temporal instability is detected for heights exceeding 25% of the undisturbed boundary-layer thickness, or one unit of the undisturbed displacement thickness at the step chordwise location. Forward-facing steps with the greatest height are not found to be temporally unstable in contrast to back...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between two-dimensional steps and gaps with stationary crossflow vortices on a swept ...
The effects of forward- and backward-facing steps on the receptivity and stability of three-dimensio...
The destabilisation effects of forward and backward facing steps on cross-flow (CF) disturbances on ...
A low-speed experiment was performed on a swept at plate model with an imposed pressure gradient to ...
Destabilisation effects of forward facing steps, backward facing steps and bumps on stationary and t...
The location of laminar to turbulent transition is an important consideration as turbulent flow is a...
Maintaining laminar flow and delaying transition to turbulence on aircraft wings reduces friction dr...
The effect of forward-facing step shape on stationary-crossflow growth was studied downstream of a t...
We study the interaction between a stationary crossflow instability and forward-facing steps in a sw...
An experimental investigation was carried out to examine the effect of two-dimensional Forward Facin...
The development of secondary instabilities in a boundary layer over a backward-facing step is invest...
An experimental investigation was carried out to examine the effect of two-dimensional Forward Facin...
The problem of identification and verification of the most important linear stability mechanisms of ...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between two-dimensional steps and gaps with stationary crossflow vortices on a swept ...
The effects of forward- and backward-facing steps on the receptivity and stability of three-dimensio...
The destabilisation effects of forward and backward facing steps on cross-flow (CF) disturbances on ...
A low-speed experiment was performed on a swept at plate model with an imposed pressure gradient to ...
Destabilisation effects of forward facing steps, backward facing steps and bumps on stationary and t...
The location of laminar to turbulent transition is an important consideration as turbulent flow is a...
Maintaining laminar flow and delaying transition to turbulence on aircraft wings reduces friction dr...
The effect of forward-facing step shape on stationary-crossflow growth was studied downstream of a t...
We study the interaction between a stationary crossflow instability and forward-facing steps in a sw...
An experimental investigation was carried out to examine the effect of two-dimensional Forward Facin...
The development of secondary instabilities in a boundary layer over a backward-facing step is invest...
An experimental investigation was carried out to examine the effect of two-dimensional Forward Facin...
The problem of identification and verification of the most important linear stability mechanisms of ...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between forward-facing steps of several heights and a pre-existing critical stationa...
The interaction between two-dimensional steps and gaps with stationary crossflow vortices on a swept ...