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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    U S Naval Research Laboratory -- Shock and Vibration Bul


    Contributors:


    Publication date :

    1967


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Launch vehicle aerodynamic flight test results

    Gaines, L. M. / Osborn, W. L. / Wiltse, P. D. | NTRS | 1983


    Structural response to inflight acoustic and aerodynamic environments

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


    Structural Response to Inflight Acoustic and Aerodynamic Environments

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


    Launch Vehicle Performance Enhancement Using Aerodynamic Lifting During Early Flight

    McDavid, B. / Hartfield, R. / Burkhalter, J. et al. | British Library Conference Proceedings | 2008


    Post-Flight Estimation of Aerodynamic Angles for a Launch Vehicle

    D'Antuono, Vincenzo / Zavoli, Alessandro / De Matteis, Guido et al. | AIAA | 2024