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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
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DOI: https://doi.org/10.15372/PMTF20220110
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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