Aeroelastic stability of a sandwich shell supported by annular ribs and a cylinder
- Authors: Bakulin V.N.1, Nedbai A.Y.2
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Affiliations:
- Institute of Applied Mechanics, Russian Academy of Sciences
- Corporation “Moscow Institute of Thermal Engineering”
- Issue: Vol 516, No 1 (2024)
- Pages: 39-46
- Section: МЕХАНИКА
- URL: https://rjmseer.com/2686-7400/article/view/651784
- DOI: https://doi.org/10.31857/S2686740024030068
- EDN: https://elibrary.ru/KAATVI
- ID: 651784
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Note
Presented by Academician of the RAS A.M. Lipanov