Development eliminates problems associated with prohibitive number of possible system modes for fluttering compressor or turbine blade row; existence and uniqueness of extremely simple system flutter modes are proved for blade rows consisting of identical blades equally spaced about common rotor.


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    Title :

    System mode shapes in flutter of compressor blade rows


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Lane, F. (author)


    Publication date :

    1956


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :