Abstract
The inductive reactance of a flat and rigid wing performing harmonic oscillations with a sufficiently large amplitude at an arbitrary position of the axis of rotation was estimated. In the plane problem, analytical expressions for the components of inductive reactance through the coefficients of hydrodynamic derivatives for harmonic variations in the angle of attack were obtained.
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Original Russian Text © E.V. Romanenko, S.G. Pushkov, V.N. Lopatin, 2012, published in Uspekhi Sovremennoi Biologii, 2012, Vol. 132, No. 6, pp. 611–624.
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Romanenko, E.V., Pushkov, S.G. & Lopatin, V.N. Inductive reactance of a rigid wing at harmonic linear oscillations and angle of attack. Biol Bull Rev 3, 176–185 (2013). https://doi.org/10.1134/S2079086413020072
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DOI: https://doi.org/10.1134/S2079086413020072