Stability and control systems adopted by Bell Aircraft Corp and for Short S.C.1 are discussed with regard to efficiency; importance of low loss nozzle systems; form of auto stabilization and its application to aircraft control system are governed by operating requirements of VTOL aircraft; lift engine intake problems and interaction effects of airflow passing through lift engines on airframe are considered; ground effects and novel model testing techniques, future research needed.


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    Titel :

    Aerodynamic design problems of jet lift V.T.O.L. Aircraft


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Fletcher, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Prospects for civil V.T.O.L. Aircraft

    Chichester-Miles, I. | Engineering Index Backfile | 1966


    The Prospects for Civil V.T.O.L. Aircraft

    Chichester-Miles, Ian | Emerald Group Publishing | 1966


    Aerodynamic Design Problems of Jet Lift V.T.O.L Aircraft

    Fletcher, J. | Emerald Group Publishing | 1962


    AIRCRAFT WITH AERODYNAMIC LIFT GENERATING DEVICE

    PEEBLES PATRICK WILLIAM | Europäisches Patentamt | 2016

    Freier Zugriff

    Aerodynamic Problems of high lift

    Schlichting, Hermann | TIBKAT | 1962