Opposition control of artificially initiated turbulent spots in a laminar boundary layer was carried out in a low-turbulence wind tunnel with the aim to delay transition to turbulence by modifying the turbulent structure within the turbulent spots. The timing and duration of control, which was carried out using wall-normal jets from a spanwise slot, were pre-determined based on the baseline measurements of the transitional boundary layer. The results indicated that the high-speed region of the turbulent spots was cancelled by opposition control, which was replaced by a carpet of low-speed fluid. The application of the variable-interval time-averaging technique on the velocity fluctuation signals demonstrated a reduction in both the burst du...
Friction drag reduction is one of the main topic of investigation because of the great beneficial fa...
Laminar to turbulent transition is a critically important process in hypersonic vehicle design. High...
The present work describes a method for the computation of the nucleation rate of turbulent spots in...
Opposition control of artificially initiated turbulent spots in a laminar boundary layer was carried...
The distribution of the rate of turbulent spot formation in the boundary layer transition region alo...
Bypass transition, i.e. transition of a boundary layer at subcritical Reynolds numbers, has been stu...
In engineering applications, there is a strong desire to reduce energy losses due to turbulent energ...
Efficient methods of drag reduction in wall-bounded shear flows remains an important, yet elusive pr...
An artificial turbulent spot is simulated in a zero free-stream turbulence base flow and a base flow...
Direct numerical simulation data of bypass transition in flat-plate boundary layers are analysed to ...
Recent experimental studies of laminar-turbulent transition are presented withfocus on adverse press...
Proportional opposition control of sweep events in a turbulent boundary layer has been carried out u...
Direct numerical simulations have been performed to study the dynamics of isolated turbulent spots i...
A variety of wall turbulence control devices which were experimentally investigated are discussed; t...
Transition to turbulence in shear flows is a puzzling problem regarding the motion of fluids flowing...
Friction drag reduction is one of the main topic of investigation because of the great beneficial fa...
Laminar to turbulent transition is a critically important process in hypersonic vehicle design. High...
The present work describes a method for the computation of the nucleation rate of turbulent spots in...
Opposition control of artificially initiated turbulent spots in a laminar boundary layer was carried...
The distribution of the rate of turbulent spot formation in the boundary layer transition region alo...
Bypass transition, i.e. transition of a boundary layer at subcritical Reynolds numbers, has been stu...
In engineering applications, there is a strong desire to reduce energy losses due to turbulent energ...
Efficient methods of drag reduction in wall-bounded shear flows remains an important, yet elusive pr...
An artificial turbulent spot is simulated in a zero free-stream turbulence base flow and a base flow...
Direct numerical simulation data of bypass transition in flat-plate boundary layers are analysed to ...
Recent experimental studies of laminar-turbulent transition are presented withfocus on adverse press...
Proportional opposition control of sweep events in a turbulent boundary layer has been carried out u...
Direct numerical simulations have been performed to study the dynamics of isolated turbulent spots i...
A variety of wall turbulence control devices which were experimentally investigated are discussed; t...
Transition to turbulence in shear flows is a puzzling problem regarding the motion of fluids flowing...
Friction drag reduction is one of the main topic of investigation because of the great beneficial fa...
Laminar to turbulent transition is a critically important process in hypersonic vehicle design. High...
The present work describes a method for the computation of the nucleation rate of turbulent spots in...