THE TABLES I, II and II which have to be read in conjunction with figs. 4, 5 and 6, show the structure of each class of stability boundary regarded as a function of the parameter Y. The end column marked ‘N’ indicates the number of real points of the boundary arising from each value of Y in the range considered. On each boundary the arrows indicate the way in which the curve is traced out as Y increases from zero to infinity.
Simplified Helicopter Ground Resonance Stability Boundaries
Development of a New Method of Determining Stability Boundaries
Aircraft Engineering and Aerospace Technology ; 34 , 11 ; 332-334
1962-11-01
3 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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