Account of STOL aircraft, developed by De Havilland Aircraft of Canada, starting with bush aircraft Beaver in which short takeoff and landing performance was one of most important considerations in design; military use of Otter fitted with 600 hp R1340 geared Wasp engine; DHC-4 Caribou fitted with two R2000 engines of 1450 hp each; research vehicle to study aerodynamic, performance, stability and control problems associated with STOL aircraft and future projects.


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    Titel :

    Development of STOL airplane


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    V/STOL cargo airplane characteristics

    Garrard, W.C.J. | Engineering Index Backfile | 1961


    Preliminary design of "ARAVA" STOL airplane

    Mankuta, H. / Sa'Ar, D. | Engineering Index Backfile | 1967


    Commercial STOL - The Airplane, the Airport

    Davy, M. C. W. | SAE Technical Papers | 1978


    Fan inlet for a V/STOL airplane

    Koncsek, J. L. / Syberg, J. | NTRS | 1977


    Design of a V/STOL technology airplane

    Zabinsky, J. M. / Burnham, R. W. | NTRS | 1975