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Temporal representations of the coefficients of aerodynamic forces and moments experienced by a rectangular wing under conditions of static hysteresis

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Abstract

Results are presented of experimental investigations into the static hysteresis of the aerodynamic characteristics of a rectangular wing with an aspect ratio of λ=5, obtained in static tests of a wing model in a wind tunnel. Variation with time of the aerodynamic forces and moments are analyzed in the range of angles of attack where a transition occurs from one branch of the hysteresis loop to the other.

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Authors
  1. I. V. Kolin
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  2. T. I. Trifonov
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  3. D. V. Shukhovtsov
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Additional information

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Translated from Zhurnal Tekhnichesko\(\overset{\lower0.5em\hbox{$\smash{\scriptscriptstyle\smile}$}}{l}\) Fiziki, Vol. 71, No. 7, 2001, pp. 128–132.

Original Russian Text Copyright © 2001 by Kolin, Trifonov, Shukhovtsov.

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Kolin, I.V., Trifonov, T.I. & Shukhovtsov, D.V. Temporal representations of the coefficients of aerodynamic forces and moments experienced by a rectangular wing under conditions of static hysteresis. Tech. Phys. 46, 914–918 (2001). https://doi.org/10.1134/1.1387557

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  • DOI: https://doi.org/10.1134/1.1387557

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