A modified wing with the long core separate flow nacelle and several E(3) nacelles was utilized. The effects of nacelle and pylon cant angles and nacelle longitudinal and vertical location were investigated over a Mach number range from 0.70 to 0.83. The results at the cruise condition 0.82 Mach number and 0.55 lift coefficient are presented.


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    Title :

    Investigation of powered nacelles on a high aspect ratio NASA supercritical wing, phase 2


    Contributors:


    Publication date :

    1981-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English