Applications of methods in determination of dynamic loadings and response for both aircraft and missiles subject to continuous turbulence; input transfer function output relationships and procedure whereby mission design load information may be obtained utilizing digital computer; applications to problem areas such as determination of design fin load, evaluation of crew station accelerations for low level high speed operation, and missile gust loads in terminal dive condition.


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    Title :

    Application of power spectral methods in airplane and missile design


    Additional title:

    J Aero/Space Sciences


    Contributors:
    Thorson, K.R. (author) / Bohne, Q.R. (author)

    Published in:

    Journal of Aerospace Science ; 27 , n 2 ; p 107-116


    Publication date :

    1960


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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