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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Nozzles for jet-lift V/Stol aircraft


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1967


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    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