Paper deals with effect on aircraft design of some of operating parameters, in particular its operational takeoff characteristics when overloaded; data reported show that military VTOL aircraft is limited to short ranges and small loads; curves show effects of power loading and wing lift on takeoff performance; it is suggested that variable sweep wing will overcome conflicting requirements; variation of interference effects with engine position and forward speed is shown; pilot techniques used during short takeoff and some of engineering work carried out on variables sweep wings.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    STOL capabilities of VTOL aircraft -- Some operating parameters


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Boorer, N.W. (Autor:in) / Davey, B.J. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 VTOL-STOL



    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    STOL Capabilities of VTOL Aircraft – Some Operating Parameters

    Davey, B. J. / Boorer, N. W. | SAE Technical Papers | 1964


    VTOL-STOL aircraft

    Engineering Index Backfile | 1956


    VTOL-STOL aircraft

    Bock, G. / Spintzyk, H. | Engineering Index Backfile | 1961


    VTOL-STOL

    Engineering Index Backfile | 1960


    Performance of STOL- and VTOL-aircraft

    Wittenberg, H. | Engineering Index Backfile | 1960