Wind-tunnel data of effects of split flaps; structural tests of series of stiffened sheet metal panels in edge compression; comparison of 15 types of stiffeners suitable for use on reinforced sheet structures subjected to compression; results of flight tests and theoretical studies combined with wind tunnel tests of airfoils.


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    Title :

    Technological developments of curtiss-wright coupe


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1936


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Curtiss-Wright Model 19L Coupe

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