Testing at Boeing has progressed from simple half wing cantilever model of 1946 to almost completely scaled flutter models tested in simulation of free flight; continued development of analysis techniques and correlation with full scale flight testing needed for more accurate predictions of flutter characteristics of airplane prior to final design of flight stages.


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    Titel :

    Flutter analysis of complex airplanes by experimental methods


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Kinnaman, E.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1952


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Flutter Problems of Business Airplanes

    McKillop, J. A. | SAE Technical Papers | 1965


    Safeguards Against Flutter of Airplanes

    deVries, Gerhard | NTRS | 1956


    Safeguards against flutter of airplanes

    De Vries, G. | Engineering Index Backfile | 1956


    Flutter problems of business airplanes

    McKillop, J.A. | Engineering Index Backfile | 1965


    The propeller flutter problem for high-speed airplanes

    Baker, J. E. / Regier, A. A. | NTRS | 1949