Unified system of procedures is developed for estimating some important classes of in-flight noise environments and resulting surface vibration on typical launch vehicle; noise environments are classified according to nature of spatial and temporal correlations of associated fluctuating pressure fields; structural elements considered are cylinder and flat plate; some numerical examples are presented for estimates of frequency spectra of acceleration on vibrating structures; applicable also to orthotropic and liquid-loaded structures.


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    Titel :

    Response of structural components of launch vehicle to in-flight acoustic and aerodynamic environments


    Weitere Titelangaben:

    U S Naval Research Laboratory -- Shock and Vibration Bul


    Beteiligte:
    Chandiramani, K.L. (Autor:in) / Lyon, R.H. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Structural Response to Inflight Acoustic and Aerodynamic Environments

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    Structural response to inflight acoustic and aerodynamic environments

    Chandiramani, K. L. / Franken, P. A. / Lyon, R. H. et al. | NTRS | 1967


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