Review of 4-yr STOL Research Program conducted jointly by DeHavilland Aircraft of Canada and Canadian Defence Research Board; Otter aircraft which employs powerful double slotted flaps is fitted with enlarged flaps with novel aerodynamic features and used in studies to assess static stability and control problems; boundary layer control scheme adapted to requirement of flight aircraft; performance and stability tests, flight test and results.


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    Title :

    Towards still shorter takeoffs and landings


    Additional title:

    Can Aeronautical J


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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