Existence of flutter in such craft depends, in part, on dynamic characteristics of servomechanism used for control; method evolved wherein impedance of servo and related elastic structure, as obtained by test, is compared to set of theoretical flutter boundary curves.
Flutter of servo-controlled aircraft
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 16 , n 7
1949
8 pages
Charts
Article (Journal)
English
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