Author: J. B. Abbiss
Publisher:
ISBN:
Category : Laser Doppler velocimeter
Languages : en
Pages : 22
Book Description
Experiments with a three-component laser anemometer on the wake and vortex structure behind a model wing at incidence in a 4ft x 3ft subsonic test section are described. Three colours from the output spectrum of an argon-ion laser were used for the three Doppler-difference arrangements. The complete optical system operated in backscatter and was mounted on a single table which could be translated in three orthogonal directions. An integrated data acquisition and reduction system was used incorporating a photon correlator and a Honeywell 6/36 minicomputer. The output data consisted of mean-velocity and turbulence-intensity values for all three components at each measurement point. From these data, the mean-velocity components in the directions of the conventional tunnel axes could be derived by means of a linear transformation. However, the measured turbulence intensities do not yield the turbulence intensities for these components without additional assumptions or supplementary information. (Author).
Experiments Using a Three-Component Laser-Anemometry System on a Subsonic Flow with Vorticity
Author: J. B. Abbiss
Publisher:
ISBN:
Category : Laser Doppler velocimeter
Languages : en
Pages : 22
Book Description
Experiments with a three-component laser anemometer on the wake and vortex structure behind a model wing at incidence in a 4ft x 3ft subsonic test section are described. Three colours from the output spectrum of an argon-ion laser were used for the three Doppler-difference arrangements. The complete optical system operated in backscatter and was mounted on a single table which could be translated in three orthogonal directions. An integrated data acquisition and reduction system was used incorporating a photon correlator and a Honeywell 6/36 minicomputer. The output data consisted of mean-velocity and turbulence-intensity values for all three components at each measurement point. From these data, the mean-velocity components in the directions of the conventional tunnel axes could be derived by means of a linear transformation. However, the measured turbulence intensities do not yield the turbulence intensities for these components without additional assumptions or supplementary information. (Author).
Publisher:
ISBN:
Category : Laser Doppler velocimeter
Languages : en
Pages : 22
Book Description
Experiments with a three-component laser anemometer on the wake and vortex structure behind a model wing at incidence in a 4ft x 3ft subsonic test section are described. Three colours from the output spectrum of an argon-ion laser were used for the three Doppler-difference arrangements. The complete optical system operated in backscatter and was mounted on a single table which could be translated in three orthogonal directions. An integrated data acquisition and reduction system was used incorporating a photon correlator and a Honeywell 6/36 minicomputer. The output data consisted of mean-velocity and turbulence-intensity values for all three components at each measurement point. From these data, the mean-velocity components in the directions of the conventional tunnel axes could be derived by means of a linear transformation. However, the measured turbulence intensities do not yield the turbulence intensities for these components without additional assumptions or supplementary information. (Author).
Scientific and Technical Aerospace Reports
Technical Abstract Bulletin
Performance and Analysis of a Three-dimensional Nonorthogonal Laser Doppler Anemometer
Aircraft Wake Vortices
Author: James N. Hallock
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 396
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 396
Book Description