Design considerations for short haul aircraft that will take off vertically yet fly with forward speeds considerably greater than those now possible with helicopters; fuselage must remain horizontal while on ground and in all flight regimes, from hovering or low speed flight to maximum speed; controllability, stability and general safety requirements cannot be compromised; table shows short haul transport comparative study for tilt wing propeller and tandem helicopter.


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    Titel :

    Tilt-wing VTOL aircraft


    Weitere Titelangaben:

    Shell Aviation News


    Beteiligte:
    McCormick, Jr., B.W. (Autor:in) / Mallen, J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Tilt-wing VTOL aircraft as commercial air transport

    Mazzitelli, F.R. | Engineering Index Backfile | 1957


    Tilt-wing VTOL aircraft as commercial air transport

    Mazzitelli, F.R. | Engineering Index Backfile | 1957


    Some aeroelastic problems of tilt-wing VTOL aircraft

    Loewy, R.G. / Yntsma, R.T. | Engineering Index Backfile | 1958



    Product analysis of tilt-wing propelloplane type VTOL aircraft

    Nichols, J.B. | Engineering Index Backfile | 1959