To deflect exhaust of V/STOL aircraft fan deploy set of rectangular flaps so exhaust stream can be turned as required and then directed through exit nozzles which generate thrust in appropriate direction; lateral deflection of exhaust is provided by yaw vanes.


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    Titel :

    Thrust vector control for V/STOL aircraft


    Beteiligte:
    Toney, E. W. (Autor:in)

    Erscheinungsdatum :

    01.05.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Thrust Reversers for Civil STOL Aircraft

    Sutton, J. M. D. / Colley, R. H. | SAE Technical Papers | 1973


    Thrust vector control of a V/STOL airship

    NAGABHUSHAN, B. L. / FAISS, G. D. | AIAA | 1984


    Ejector thrust augmentation for STOL aircraft applications

    STREIFF, H. / HENDERSON, C. | AIAA | 1974


    Optimum Lift/Thrust System for V/STOL Aircraft

    Dev, S.P. | British Library Conference Proceedings | 2008