Add to ORKGIn the closer investigation of the results obtained from a wing model with a rotary cylinder mounted in its leading edge (NACA TM's 307 and 354), the velocity distribution in the vicinity of the surface of the model was determined by a hot-wire anemometer. The results confirmed the belief that the rotary cylinder had considerable effect on the air flow, but demonstrated the fact that the direct influence of the cylinder is confined to a very thin layer in immediate proximity to the surface
The published data on the distribution of speed near a thin flat plate with sharp leading edge place...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
The results of the velocity measurements in the boundary layer described in NACA-TM 411 are here dis...
In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted...
The speed distribution in a laminar boundary layer on the surface of an elliptic cylinder, of major ...
The concept of moving surface boundary-layer control, as applied to the Joukowsky and NACA airfoils,...
Into the leading edge of a wing with arbitrary cross-section, there is introduced a cylinder, which ...
Tests were made in the no. 1 wind tunnel at Langley Memorial Aeronautical Laboratory to determine th...
The study of boundary layer separation control using cylinder based at the leading edge o...
The boundary layer of an elliptic cylinder of major and minor axis 11.78 and 3.98 inches, respective...
The concept of Moving Surface Boundary-layer Control (MSBC), as applied to a two-dimensional Joukow...
The object of the present investigation is to determine the velocity in the BMW-VI cylinder of an ex...
Tests have been made at high speeds to determine the drag of models, simulating propeller shanks, in...
The interaction between the wake of a rotor blade and a downstream cylinder holds the key to the und...
The published data on the distribution of speed near a thin flat plate with sharp leading edge place...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...
The results of the velocity measurements in the boundary layer described in NACA-TM 411 are here dis...
In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted...
The speed distribution in a laminar boundary layer on the surface of an elliptic cylinder, of major ...
The concept of moving surface boundary-layer control, as applied to the Joukowsky and NACA airfoils,...
Into the leading edge of a wing with arbitrary cross-section, there is introduced a cylinder, which ...
Tests were made in the no. 1 wind tunnel at Langley Memorial Aeronautical Laboratory to determine th...
The study of boundary layer separation control using cylinder based at the leading edge o...
The boundary layer of an elliptic cylinder of major and minor axis 11.78 and 3.98 inches, respective...
The concept of Moving Surface Boundary-layer Control (MSBC), as applied to a two-dimensional Joukow...
The object of the present investigation is to determine the velocity in the BMW-VI cylinder of an ex...
Tests have been made at high speeds to determine the drag of models, simulating propeller shanks, in...
The interaction between the wake of a rotor blade and a downstream cylinder holds the key to the und...
The published data on the distribution of speed near a thin flat plate with sharp leading edge place...
An experimental investigation of the transverse curvature effect on laminar and turbulent axially s...
This report describes test made in the Variable Density Wind Tunnel of the NACA to determine the pos...