The optical, seeding, and data reduction procedures which have been used in the successful application of laser velocimetry to large-scale, unsteady, transonic wind-tunnel testing are described. Flowfield measurements obtained at several facilities are presented. These results include vortex flow measurements and ensemble-averaged data obtained under conditions of vortex-shedding, dynamic stall airfoil oscillation, oscillating trailing-edge control flaps, and helicopter rotor flow fields.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Application of laser velocimetry to unsteady flows in large scale, high speed tunnels


    Contributors:
    Owen, F. K. (author)

    Publication date :

    1983-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Laser Velocimetry In Low-Speed Wind Tunnels

    Orloff, Kenneth L. / Snyder, Philip K. / Reinath, Michael S. | NTRS | 1990


    Spatial correlation velocimetry in unsteady flows

    FAWCETT, P. / KOMERATH, N. | AIAA | 1991


    Advances in Planar Doppler Velocimetry for Large-Scale Wind Tunnels

    McKenzie, R. L. / Reinath, M. S. / Jenkins, T. P. et al. | British Library Conference Proceedings | 2004


    Advances in Planar Doppler Velocimetry for Large-Scale Wind Tunnels

    McKenzie, Robert / Reinath, Michael / Jenkins, Thomas | AIAA | 2004