Effect of Northrop and Zap trailing-edge flaps on airplane performance, by deflecting flaps 15-20° on take-off run of Northrop monoplane is reduced by about 30%; weight of Zap installation with operating mechanism is approximately 0.3 to 0.36 lb per sq ft of wing area.


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    Title :

    Split trailing-edge flap


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 44 , n 9


    Publication date :

    1933


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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