Results of some of developments, carried out recently by de Havilland Aircraft of Canada Ltd, are presented with respect to basic STOL performance, and low-speed control and handling; classical STOL deflected slipstream configuration and some of its limitations are reviewed; some improvements to basic design approach and in longitudinal low-speed control are discussed; other criteria are reviewed; flight-test results obtained with experimental aircraft incorporating modified longitudinal control system are discussed.


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    Titel :

    Some recent aerodynamic advances in STOL aircraft


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Johnston, G.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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