SAE-G-5 Aerospace Shock and Vibration Committee was formed to establish stepwise procedure for design of linear, center-of-gravity type vibration isolation systems whose function is to protect fragile equipment, installed on aircraft, missiles or spacecraft, from sinusoidal and random vibrational environments encountered; publication presents philosophy and approach applied, general concepts, concept of vibration source, fragility, outline of theoretical background, and practical application.


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    Titel :

    Rational procedure for design of vibration isolation systems


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Molloy, C.T. (Autor:in) / Mintz, F. (Autor:in) / Harter, W.W. (Autor:in) / Safford, F.B. (Autor:in) / Rubin, S. (Autor:in) / Mustain, R.W. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    28 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    A rational procedure for the design of vibration isolation systems

    Society of Automotive Engineers | TIBKAT | 1961



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