The influence of suction on step-induced boundary-layer transition has been experimentally investigated in the Cryogenic Ludwieg-Tube Goettingen at large chord Reynolds numbers (up to 16·106), Mach numbers from 0.35 to 0.77 and various streamwise pressure gradients by means of temperature-sensitive paint. Surface imperfections, implemented as combination of gap and forward-facing step, caused transition to occur at a location more upstream than in the case of a smooth surface (i.e. without gap and step). For this combination of imperfections, it was demonstrated for the first time in experiments that suction, achieved passively by exploiting the pressure difference between upper and lower side of the model, induced a movement of transition ...
Practical laminar flow wing design requires joints, panels and high-lift devices, but steps and/or g...
The influence of surface bumps on boundary-layer transition was experimentally investigated in the p...
The projected increase in air traffic volume has led to a renewed interest in drag reduction researc...
The influence of suction on step-induced boundary-layer transition has been experimentally investiga...
The influence of suction on step-induced boundary-layer transition has been experimentally investiga...
Laminar flow on transport aircraft is challenging to maintain in the presence of surface imperfectio...
The influence of suction on gap- and step-induced boundary-layer transition was investigated experim...
In the scope of this master thesis, a systematic experimental investigation of the delay of step-ind...
The effect of sharp forward-facing steps on boundary-layer transition is systematically investigated...
AbstractThe effect of geometric forward-facing steps on boundary layer transition was experimentally...
Experiments were conducted at a subsonic Mach number in the Cryogenic Ludwieg-Tube Göttingen to stud...
The effect of geometric forward-facing steps on boundary layer transition was experimentally investi...
Experiments were conducted up to high subsonic Mach number in the Cryogenic Ludwieg-Tube Göttingen t...
The effect of sharp forward-facing steps on boundary-layer transition was systematically investigate...
The effect of sharp forward-facing steps and sinusoidal bumps on boundary-layer transition was syste...
Practical laminar flow wing design requires joints, panels and high-lift devices, but steps and/or g...
The influence of surface bumps on boundary-layer transition was experimentally investigated in the p...
The projected increase in air traffic volume has led to a renewed interest in drag reduction researc...
The influence of suction on step-induced boundary-layer transition has been experimentally investiga...
The influence of suction on step-induced boundary-layer transition has been experimentally investiga...
Laminar flow on transport aircraft is challenging to maintain in the presence of surface imperfectio...
The influence of suction on gap- and step-induced boundary-layer transition was investigated experim...
In the scope of this master thesis, a systematic experimental investigation of the delay of step-ind...
The effect of sharp forward-facing steps on boundary-layer transition is systematically investigated...
AbstractThe effect of geometric forward-facing steps on boundary layer transition was experimentally...
Experiments were conducted at a subsonic Mach number in the Cryogenic Ludwieg-Tube Göttingen to stud...
The effect of geometric forward-facing steps on boundary layer transition was experimentally investi...
Experiments were conducted up to high subsonic Mach number in the Cryogenic Ludwieg-Tube Göttingen t...
The effect of sharp forward-facing steps on boundary-layer transition was systematically investigate...
The effect of sharp forward-facing steps and sinusoidal bumps on boundary-layer transition was syste...
Practical laminar flow wing design requires joints, panels and high-lift devices, but steps and/or g...
The influence of surface bumps on boundary-layer transition was experimentally investigated in the p...
The projected increase in air traffic volume has led to a renewed interest in drag reduction researc...