Elastic model wings and flutter recorders; comparative investigation of influence of angle of attack, elastic properties, distribution of masses of mutual frequencies, location of center of gravity of aileron and elasticity of control and influence of wing support; comparison of results and values calculated according to Blenk and Lieber's method are given. Communication from German Experimental Laboratory for Aviation D. V. L.


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    Title :

    Investigation of wing flutter in the wind tunnel


    Additional title:

    Untersuchung von Fluegelschwingungen im Windkanal


    Contributors:
    Essers, I. (author)

    Published in:

    Publication date :

    1929


    Size :

    26 pages


    Remarks:

    30 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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