Experimental studies of the impact of fluid sloshing in the tank on the dynamic characteristics of the “wing model – fuel tank” system

Flexible response of the airframe structural elements under operational loads are one of the main sources of fatigue damage accumulation. It is known that fuel sloshing in tanks can change the dynamic (frequencies and shapes of natural oscillations) and dissipative properties (oscillation damping de...

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Bibliographic Details
Main Authors: G. B. Vardanyan, A. S. Kochetov, Y. V. Petrov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2024-05-01
Series:Научный вестник МГТУ ГА
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Online Access:https://avia.mstuca.ru/jour/article/view/2336
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