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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    Title :

    Some recent aerodynamic advances in STOL aircraft


    Additional title:

    J Aircraft


    Contributors:

    Published in:

    Publication date :

    1965


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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