A brief summary of recent 40- by 80-foot wind-tunnel investigations of large-scale models equipped with various high-lift devices is presented. The basic high-lift concepts that were investigated were the externally blown flap, the augmentor wing, and the rotating-cylinder flap. The scope of this paper is limited to a discussion of the wind-tunnel results in terms of maximum lift, descent performance, and pitch trim requirements.


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    Title :

    A summary of recent large-scale research on high-lift devices


    Contributors:

    Conference:

    Conference on V/STOL and STOL aircraft ; 1966 ; Mountain View, CA, US


    Published in:

    Publication date :

    1966-04-04


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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