Analysis of stabilizing fin at Mach numbers from 2 to 7 was performed, based on preassigned mode shapes with piston theory representing aerodynamic forces; eigenvalues of various dynamic systems were determined for flight cases along given trajectory and for hypothetical flight cases to establish flutter boundary; for 2-mode systems eigenvalues were determined analytically; for systems with more than 2 modes iterative procedure was developed to determine eigenvalues.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flutter analysis of rocket fin at high Mach numbers


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Ohman, L.H. (Autor:in) / Dixon, R.C. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :