The report addresses the application of cold thrust augmentation - i.e., the ejector flap - to the STOL requirement. The approach is to examine the results of a preliminary analysis in light of new information which was not originally considered. The original preliminary analysis, examined the potential of this concept by 'modifying' an existing aircraft design to accept an ejector flap mechanism. It was found that in addition to an increase in STOL performance, the device could also yield performance gains by leaving the ejector flap 'on' during other flight modes, i.e., climb, loiter and cruise. The optimum ejector geometry was in the low area ratio, low thrust augmentation ratio region. This latter finding was in direct contrast to other ejector efforts of current interest. The conclusion drawn is that this concept will probably yield most benefit for STOL missions requiring extended loitering of climbing time. 'Ejector on' operation does not look promising for high speed cruise. (Author Modified Abstract)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Problem Definition for the Ejector Flap STOL Concept


    Contributors:

    Publication date :

    1972


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    A new ejector concept for V/STOL aircraft

    CHU, C.-W. / ORTIZ, V. / WIDYNSKI, T. | AIAA | 1983


    V-STOL Ejector Short Diffuser Study

    R. M. O'Donnell / R. A. Squyers | NTIS | 1976


    STOL Tactical Aircraft Investigation -- Externally Blown Flap. Volume I. Configuration Definition

    H. G. Owens / R. S. Kaneshiro / D. J. Renselaer et al. | NTIS | 1973



    Entrainment method for V/STOL ejector analysis

    BEVILAQUA, P. / MCCULLOUGH, J. | AIAA | 1976