Review of several types of nozzles for lift and lift/cruise engines; model test data are presented for short nonvectoring plug type, and simple, hemispherical-plug, vectoring nozzle; it was found that thrust and discharge coefficients obtained with simple vectoring nozzle were substantially independent of flow-deflection angle; it is shown that attempts to shorten and lighten lift-engine nozzles by eliminating whirl-removing surfaces may incur severe performance penalties; oblique-joint, elliptical shape nozzle for vectoring lift/cruise engine thrust is described and test data obtained with homogeneous flow are presented and conclusions drawn.


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    Titel :

    Nozzles for jet-lift V/Stol aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Nozzles for jet-lift V/STOL aircraft.

    KENTFIELD, J. A. C. | AIAA | 1967


    High Lift Techniques for STOL Aircraft

    Cornish, J. J. / Tanner, R. F. | SAE Technical Papers | 1967


    Fan Lift-Cruise V/STOL Aircraft

    J. M. Peterson | NTIS | 1976


    Powered lift aerodynamics of USB STOL aircraft

    MAITA, M. / FUJIEDA, H. / MORITA, M. et al. | AIAA | 1983


    Aerodynamics of lift fan V/STOL aircraft

    Kirk, J. V. / Hall, L. P. / Hodder, B. K. | NTRS | 1971