Experimental studies of the impact of fluid sloshing in the tank on the dynamic characteristics of the “wing model – fuel tank” system | Vardanyan | Civil Aviation High Technologies

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

eng | рус

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Vardanyan G.B., Kochetov A.S., Petrov Y.V. Experimental studies of the impact of fluid sloshing in the tank on the dynamic characteristics of the “wing model – fuel tank” system. Civil Aviation High Technologies. 2024;27(2):60-68. https://doi.org/10.26467/2079-0619-2024-27-2-60-68

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ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Eliseev B.P.

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About the Authors

G. B. Vardanyan
The Moscow State Technical University of Civil Aviation
Russian Federation

Georgiy B. Vardanyan, Candidate of Technical Sciences, Associate Professor of the Technical Mechanics and Engineering Graphics Chair

Moscow

A. S. Kochetov
The Moscow State Technical University of Civil Aviation
Russian Federation

Aleksander S. Kochetov, Candidate of Technical Sciences, Associate Professor of the Technical Mechanics and Engineering Graphics Chair

Moscow

Y. V. Petrov
The Moscow State Technical University of Civil Aviation
Russian Federation

Yuriy V. Petrov, Doctor of Technical Sciences, Professor, The Head of the Technical Mechanics and Engineering Graphics Chair

Moscow

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