The invention relates to aircraft wings in which there is combined therewith a jet propulsion means with thrust augmentation and in which the induced mass flow is derived from airflow over the wing surface including the boundary layer.


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    Title :

    Wing and Thrust Augmentor


    Contributors:

    Publication date :

    1971


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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