M. Zichenkov, A. Chizhov, S. Kuzmina, F. Ishmuratov, A. Zubakov

DOI Number: N/A

Conference number: IFASD-2017-043

An effective method is developed for analyzing of flutter characteristics of the aircraft with control system taking into account unsteadiness of aerodynamic forces. The application of the method is demonstrated for typical examples of regional aircraft with engines under wing and maneuverable aircraft with container on the wing tip.

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In Categories: 1.Events, Aeroservoelasticity, IFASD 2017
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