The Tollmien-Schlichting (TS) instability is a time-dependence instability which can lead to transition of laminar boundary layers on airfoils. A comparison of theoretical predictions and experimental observations of the TS instability on the NLF(1)-0414F airfoil designed by Viken and Pfenninger. The theoretical predictions were obtained using the SALLY stability code. Test results, from the same hot films that were used to detect transition, revealed that TS waves could be detected by the hot films if the hot-film signal was adequately modified
The laminar-turbulent transition on an airfoil can be delayed by active control of Tollmien Schlicht...
Acoustic receptivity to Tollmien-Schlichting waves in the presence of surface roughness is investiga...
This work presents an experimental and numerical investigation jointly conducted by TU Delft and DLR...
So far, very little is known about instability wave propagation in a wing boundary layer in free fli...
Flight tests were performed in order to learn more about the technically important case of naturally...
In 2001, flight tests were performed in order to learn more about boundary layer transition induced ...
The effect of long-wavelength sinusoidal surface waviness on the development of Tollmien-Schlichting...
In the present work, experimental tests are conducted to study boundary layer transition over a supe...
The paper is devoted to an experimental study of the effect of a shallow 3D roughness element on the...
Extensive combined experimental and theoretical investigations of the linear evolution of three-dime...
A new technique using surface-film activators has been developed to induce and control laminar-insta...
Understanding, predicting and controlling laminar to turbulent transition is of great interest due t...
Current manufacturing techniques in the aviation industry result in a number of two-dimensional surf...
AbstractThe goal of this study is a numerical investigation of the effect of rippled surfaces on tra...
Experiments are conducted in the Arizona State University Unsteady Wind Tunnel to investigate acoust...
The laminar-turbulent transition on an airfoil can be delayed by active control of Tollmien Schlicht...
Acoustic receptivity to Tollmien-Schlichting waves in the presence of surface roughness is investiga...
This work presents an experimental and numerical investigation jointly conducted by TU Delft and DLR...
So far, very little is known about instability wave propagation in a wing boundary layer in free fli...
Flight tests were performed in order to learn more about the technically important case of naturally...
In 2001, flight tests were performed in order to learn more about boundary layer transition induced ...
The effect of long-wavelength sinusoidal surface waviness on the development of Tollmien-Schlichting...
In the present work, experimental tests are conducted to study boundary layer transition over a supe...
The paper is devoted to an experimental study of the effect of a shallow 3D roughness element on the...
Extensive combined experimental and theoretical investigations of the linear evolution of three-dime...
A new technique using surface-film activators has been developed to induce and control laminar-insta...
Understanding, predicting and controlling laminar to turbulent transition is of great interest due t...
Current manufacturing techniques in the aviation industry result in a number of two-dimensional surf...
AbstractThe goal of this study is a numerical investigation of the effect of rippled surfaces on tra...
Experiments are conducted in the Arizona State University Unsteady Wind Tunnel to investigate acoust...
The laminar-turbulent transition on an airfoil can be delayed by active control of Tollmien Schlicht...
Acoustic receptivity to Tollmien-Schlichting waves in the presence of surface roughness is investiga...
This work presents an experimental and numerical investigation jointly conducted by TU Delft and DLR...