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.
Application of power spectral methods in airplane and missile design
J Aero/Space Sciences
Journal of Aerospace Science ; 27 , n 2 ; p 107-116
1960
10 pages
Aufsatz (Zeitschrift)
Englisch
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