A backscatter laser Doppler velocimeter which simultaneously senses the axial and the tangential components of the velocity has been used to measure the velocity distributions in the near wake of a swept wing semispan transport model in a wind tunnel. The model configuration included nacelles, pylons, antishock bodies, and wing flaps which could be deflected 27 deg. Typical wake vortex velocity profiles are presented for the flaps-retracted and the flaps-deployed 27 deg configurations, respectively.


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    Titel :

    Vortex measurements behind a swept wing transport model


    Beteiligte:
    Orloff, K. L. (Autor:in) / Ciffone, D. L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.06.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Vortex Measurements Behind a Swept Wing Transport Model

    K. L. Orloff / D. L. Ciffone | AIAA | 1974


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    Gerontakos, P. / Lee, T. | Tema Archiv | 2006


    Vortex Wake Generated Behind a Forward Swept Wing

    Lee, T. / Ko, L. S. | AIAA | 2009



    RECEPTIVITY MEASUREMENTS ON A SWEPT-WING MODEL

    Woodruff, M. / Saric, W. / Reed, H. et al. | British Library Conference Proceedings | 2011