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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2022, Volume 63, Issue 1, Pages 71–79
DOI: https://doi.org/10.15372/PMTF20220110
(Mi pmtf11)
 

Rapid flutter analysis for low-aspect-ratio wings with a control surface

M. Basiria, H. Farrokhfala, M. Mosayebia, R. Koohib

a Malek-Ashtar University of Technology, Shahinshahr, 115/83145, Iran
b Islamic Azad University, Khomeyni Shahr Branch, Khomeinishahr, 8418148499, Iran
References:
Abstract: An effective method and fast modeling in vibration and flutter analyses of low-aspect-ratio composite wings and wings with a control surface in a subsonic flow are proposed. An equivalent plate method is used for structural modeling. The doublet point and the $U$$g$ methods are applied to calculate unsteady aerodynamic loads and flutter analysis, respectively. The obtained results are in good agreement with the literature data.
Keywords: flutter, rapid analysis, low aspect ratio, control surface, doublet point method, equivalent plate method.
Received: 12.11.2020
Revised: 12.11.2020
Accepted: 28.01.2021
English version:
Journal of Applied Mechanics and Technical Physics, 2022, Volume 63, Issue 1, Pages 59–66
DOI: https://doi.org/10.1134/S0021894422010102
Bibliographic databases:
Document Type: Article
UDC: 533.6.013.42
Language: Russian
Citation: M. Basiri, H. Farrokhfal, M. Mosayebi, R. Koohi, “Rapid flutter analysis for low-aspect-ratio wings with a control surface”, Prikl. Mekh. Tekh. Fiz., 63:1 (2022), 71–79; J. Appl. Mech. Tech. Phys., 63:1 (2022), 59–66
Citation in format AMSBIB
\Bibitem{BasFarMos22}
\by M.~Basiri, H.~Farrokhfal, M.~Mosayebi, R.~Koohi
\paper Rapid flutter analysis for low-aspect-ratio wings with a control surface
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2022
\vol 63
\issue 1
\pages 71--79
\mathnet{http://mi.mathnet.ru/pmtf11}
\crossref{https://doi.org/10.15372/PMTF20220110}
\mathscinet{http://mathscinet.ams.org/mathscinet-getitem?mr=4409479}
\elib{https://elibrary.ru/item.asp?id=48064239}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2022
\vol 63
\issue 1
\pages 59--66
\crossref{https://doi.org/10.1134/S0021894422010102}
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