In program carried out by McDonnell Aircraft Corp rudder on McDonnell F-4C aircraft was selected to demonstrate advantages of beryllium application; design considerations and analysis relating to rudder design loads, balance weight loads, panel flutter, thermal environment, rudder weight, buckling and crippling criteria; fabrication and assembly of beryllium structures; rudder test program consisting of element test and rudder ground test program using Be in selected areas.


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    Titel :

    Beryllium structures for aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Barnett, F.E. (Autor:in) / Finn, J.M. (Autor:in) / Koch, L.C. (Autor:in)

    Kongress:

    SAE Meeting ; 1966 Beryllium



    Erscheinungsdatum :

    1966


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Beryllium Structures for Aircraft

    Barnett, F. E. / Finn, J. M. / Koch, L. C. | SAE Technical Papers | 1966


    Beryllium and Beryllium Metal Matrix Composite Structures

    Benoit, J. / Deutsche Gesellschaft fur Luft- und Raumfahrt / Confederation of European Aerospace Societies | British Library Conference Proceedings | 2001


    Beryllium Copper in the Aircraft Industry

    Emerald Group Publishing | 1941


    Beryllium for aerospace structures

    Riedinger, L.A. | Engineering Index Backfile | 1961


    Applications of beryllium to aircraft gas- turbine engines

    ANDREINI, G. J. / CORRIGAN, L. A. / SPAETH, C. E. | AIAA | 1964