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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    Titel :

    Wing and Thrust Augmentor


    Beteiligte:

    Erscheinungsdatum :

    1971


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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