Need for short haul commercial air transport capable of vertical takeoff and landing and having high cruising speed led to development of turboprop tilt-wing VTOL aircraft; reasons for selecting tilt-wing type; comparative study of direct operating cost of comparable helicopter and fixed wing aircraft with VTOL; comparison of block time and block speed; operational aspects; advantages and disadvantages for both commercial and military operations. (see also abstract in Soc Automotive Engrs -- J v 65 n 4 Apr 1957 p 47)


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    Titel :

    Tilt-wing VTOL aircraft as commercial air transport


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


    Beteiligte:

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1957 Vertical takeoff



    Erscheinungsdatum :

    1957


    Format / Umfang :

    17 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Tilt-wing VTOL aircraft as commercial air transport

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


    THE TILT - WING VTOL AIRCRAFT AS A COMMERCIAL AIR TRANSPORT

    Mazzitelli, F. R. | SAE Technical Papers | 1957


    Tilt-wing VTOL aircraft

    McCormick, Jr., B.W. / Mallen, J. | Engineering Index Backfile | 1957


    Some aeroelastic problems of tilt-wing VTOL aircraft

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