Novel form of flutter is explained and investigated; existence of instability is demonstrated with mathematical model of aircraft; problem is investigated by use of Lagrange's Equations of Motion and Nyquist stability criterion for servo mechanisms; method is applied to elevator system controlling pitch-plane motion of simplified aircraft having gyroscope feedback.
Flutter of aircraft controlled by automatic navigation system
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 65 , n 604
1961
6 pages
Article (Journal)
English
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