The note furnishes the free-free bending vibration modes for the XSM-65C missiles. The data presented is required for stability and loads investigations in which the effects of missile elasticity and vibration are important considerations. The bending modes for the XSM-65C missile tabulated in this report reflect a revised propellant sloshing analysis and a 33 mass station solution. An addendum is also included in which the bending vibration modes are presented for the fully tanked XSM-65C missile cantilevered at Station 1200. (Author)


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    Title :

    Natural Bending Modes of the XSM-65C Missiles at Various Instants of Flight


    Contributors:

    Publication date :

    1958


    Size :

    70 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English