The evolution of a successful distributed suction boundary layer control system is described, and an analysis of various high-lift aircraft has been performed to determine the wing lift and the increment of lift due to boundary layer control. Operational problems of distributed suction boundary layer control aircraft are discussed, and a comparison with other means of achieving similar lift coefficients is made.


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    Titel :

    Distributed Suction Boundary Layer Control for High Lift


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Roberts, S. C. (Autor:in)

    Kongress:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1968



    Erscheinungsdatum :

    01.02.1968




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Distributed suction boundary layer control for high lift

    Roberts, S.C. | Engineering Index Backfile | 1968


    Adaptive boundary layer control with distributed suction

    Rioual, J.-L. / Nelson, P. / Fisher, M. et al. | AIAA | 1993


    Adaptive Boundary Layer Control with Distributed Suction

    Rioual, J.-L. / Nelson, P. A. / Fisher, M. J. et al. | British Library Conference Proceedings | 1993