Abstract
Panel flutter theory distinguishes between two types of the loss of stability, namely, the flutter of the coupled type and the single-mode flutter. The flutter of the coupled type is well studied, both theoretically and experimentally. The single-mode flutter has been theoretically studied only quite recently. This study is devoted to the experimental investigation of the single-mode panel flutter. The fact of its generation under actual conditions is established and the stability range is determined.
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Original Russian Text © V.V. Vedeneev, S.V. Guvernyuk, A.F. Zubkov, M.E. Kolotnikov, 2010, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2010, Vol. 45, No. 2, pp. 161–175.
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Vedeneev, V.V., Guvernyuk, S.V., Zubkov, A.F. et al. Experimental investigation of single-mode panel flutter in supersonic gas flow. Fluid Dyn 45, 312–324 (2010). https://doi.org/10.1134/S001546281002016X
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DOI: https://doi.org/10.1134/S001546281002016X