A series of measurements of trailing vortices behind lifting hydrofoils is described. These measurements were made in the Caltech Free-Surface Water Tunnel, using a laser-Doppler velocimeter to measure two components of velocity in the vortex wake. Two different model planforms were tested, and measurements were made at several free-stream velocities and angles of attack for each. Velocity profiles were measured at distances downstream of the model of from five to sixty chord lengths. These measurements are the first results of a continuing experimental programme. In § 3 of this paper, the theory of trailing vortices is discussed. The effects of ‘vortex wandering’ upon the measurements are computed, and the corrected results are seen to...
As a wing produces lift it sheds vorticity into the wake in the form of a vortex sheet. Since the sh...
Since the advent of laser-Doppler anemometry (L.D.A.) as a new tool in experimental fluid mechanics ...
A brief description is given of NASA's comprehensive program to study the aircraft trailing vortex p...
A series of measurements of trailing vortices behind lifting hydrofoils is described. These measurem...
The instantaneous velocity distribution in trailing vortices generated by lifting hydrofoils has bee...
The velocity field of the trailing vortex behind a wing at different angles of attack has been measu...
Tangential and axial velocity profiles were measured in the far field wake vortices of several diffe...
Measured axial and tangential velocity profiles in the near wake vortices of a semi-span model of th...
The DFVLR laser Doppler anemometer is a CO2 continuous wave homodyne system designed for boundary la...
Activities involving the use flow visualization and laser anemometers are reviewed. In particular, t...
At high Reynolds number, the flow of an incompressible fluid over a lifting surface is a rich blend ...
At high Reynolds number, the flow of an incompressible fluid over a lifting surface is a rich blend ...
Measurements have been made in the wake of a semi-span NACA 0015 airfoil with emphasis on the region...
In the field of the fluid mechanics, the team HYDEE (Hydrodynamics and Environmental flow section) o...
A laser Doppler velocimeter whose focal volume can be rapidly traversed through a flowfield has been...
As a wing produces lift it sheds vorticity into the wake in the form of a vortex sheet. Since the sh...
Since the advent of laser-Doppler anemometry (L.D.A.) as a new tool in experimental fluid mechanics ...
A brief description is given of NASA's comprehensive program to study the aircraft trailing vortex p...
A series of measurements of trailing vortices behind lifting hydrofoils is described. These measurem...
The instantaneous velocity distribution in trailing vortices generated by lifting hydrofoils has bee...
The velocity field of the trailing vortex behind a wing at different angles of attack has been measu...
Tangential and axial velocity profiles were measured in the far field wake vortices of several diffe...
Measured axial and tangential velocity profiles in the near wake vortices of a semi-span model of th...
The DFVLR laser Doppler anemometer is a CO2 continuous wave homodyne system designed for boundary la...
Activities involving the use flow visualization and laser anemometers are reviewed. In particular, t...
At high Reynolds number, the flow of an incompressible fluid over a lifting surface is a rich blend ...
At high Reynolds number, the flow of an incompressible fluid over a lifting surface is a rich blend ...
Measurements have been made in the wake of a semi-span NACA 0015 airfoil with emphasis on the region...
In the field of the fluid mechanics, the team HYDEE (Hydrodynamics and Environmental flow section) o...
A laser Doppler velocimeter whose focal volume can be rapidly traversed through a flowfield has been...
As a wing produces lift it sheds vorticity into the wake in the form of a vortex sheet. Since the sh...
Since the advent of laser-Doppler anemometry (L.D.A.) as a new tool in experimental fluid mechanics ...
A brief description is given of NASA's comprehensive program to study the aircraft trailing vortex p...