Investigation of basic relationships which are involved in aim of obtaining further improvements; project calculations with respect to power, wing section and area; layout of design; flying characteristics and stability and control; it is concluded that laminar flow airfoil sections with built-in camber simulating small flap angle appear to be best.


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    Title :

    Design philosophy of man powered aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1962


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Aircraft design philosophy

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