Existing methods of estimating blade loadings on rotor in forward flight have suffered from necessity of using false simplifying assumptions in order to make possible analytical approach; examination of these assumptions lead to conclusion that calculation by method of elements (strip theory) gives only reliable solution.


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    Title :

    Aerodynamics of helicopter in forward flight


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :