Computer program calculates axisymmetric launch vehicle steady-state response to axisymmetric sinusoidal loads. A finite element technique is utilized to construct the total launch vehicle stiffness matrix and mass matrix by subdividing the prototype structure into a set of axisymmetric shell components, fluid components, and spring-mass components.


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    Title :

    Computer program provides improved longitudinal response analysis for axisymmetric launch vehicles


    Contributors:

    Publication date :

    1967-12-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English