Uniform flat triangular plate serves as approximation to rudimentary wing and tail surfaces on rockets, bombs, and some aircraft; there is evidence that flat plate vibrations may be correlated with actual delta wings of hollow tapered construction; in one series of plates, delta wing plan form of fixed span is maintained; in other series, fixed span and fixed root chord are maintained.


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    Titel :

    Experimental study of natural vibrations of cantilevered triangular plates


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Gustafson, P.N. (Autor:in) / Stokey, W.F. (Autor:in) / Zorowski, C.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1953


    Format / Umfang :

    7 pages


    Anmerkungen:

    Illustrations


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Airplane Vibrations Using Cantilevered Component Modes

    Schultz, William H. | SAE Technical Papers | 1968


    Airplane vibrations using cantilevered component modes

    Schultz, W.H. | Engineering Index Backfile | 1968


    Vibration Response of Cracked Cantilevered Plates Near Natural Frequency Veerings

    Saito, A. / Castanier, M. / Pierre, C. et al. | British Library Conference Proceedings | 2008


    Vibration Response of Cracked Cantilevered Plates Near Natural Frequency Veerings

    Saito, Akira / Castanier, Matthew / Pierre, Christophe | AIAA | 2008