Results of research on advanced augmentors are discussed. Research concerned with performance has indicated that: (1) augmentors with lobe-type nozzles give higher thrust augmentation than those with slot-type primary nozzles, (2) the thrust of augmentor wings at forward speed is greater than that of internally blown flaps for the speed range of interest, and (3) the optimum augmentor geometry at forward speed may be different from the optimum static geometry. Analysis of augmentor-wing data has shown that the data may be correlated by accounting for the augmentation and entrainment in defining a net thrust coefficient.


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    Titel :

    Advanced augmentor-wing research


    Beteiligte:
    Aiken, T. N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1972


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Wing and Thrust Augmentor

    H. J. P. von Ohain / W. S. Campbell | NTIS | 1971


    The Transonic Multifoil Augmentor Wing

    J.E. Farbridge / Ronald C. Smith | AIAA | 1978




    Augmentor-wing research program -- Past, present and future

    Whittley, D.C. | Engineering Index Backfile | 1968