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Method determining the nature of oscillating motion of the aircraft based on the analysis of coefficients of aerodynamic damping derivatives

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Thermophysics and Aeromechanics Aims and scope

Abstract

Analysis of experimental data shows that the nature of the oscillating motion of an aircraft does not depend uniquely on the value of the coefficients of aerodynamic damping derivatives. The present work makes an attempt to explain this phenomenon and develops a methodology to adequately characterize the oscillating motion of aircraft based on the analysis of the coefficients of aerodynamic damping derivatives.

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References

  1. K.P. Petrov, Aerodynamics of Bodies of the Simplest Shape, Faktorial, Moscow, 1998.

    Google Scholar 

  2. A.G. Reshetin, Aerodynamic hysteresis at the flow around spacecraft “Soyuz” at the hypersonic viscous mode. Results of flight experiments, Kosmonavtika i Raketostroenie, 2000, No. 19, P. 150–156

    Google Scholar 

  3. O.N. Khatuntseva, Analysis of the reasons for an aerodynamic hysteresis in flight tests of the Soyuz reentry capsule at the hypersonic segment of its descent, J. Appl. Mech. Techn. Phys., 2011, Vol. 52,No. 4, P. 544–552.

    Article  ADS  MATH  Google Scholar 

  4. O.N. Khatuntseva, Classification of hysteresis functions. Theoretical models and methods for description. E-journ. “Fiziko-himicheskaya Kinetika v Gazovoy Dinamike”, 2012, V. 13,No. 1, P. 1–23, URL: http://chemphys.edu.ru/media/files/2012-02-29-001.pdf.

    Google Scholar 

  5. A.N. Lyubimov, N.M. Tyunev, and G.I. Hut, Methods for Investigation of Gas Flow and Determination of Aerodynamic Characteristics of Axisymmetric Bodies, Nauka, Moscow, 1995.

    Google Scholar 

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Correspondence to O. N. Khatuntseva.

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Dyadkin, A.A., Khatuntseva, O.N. Method determining the nature of oscillating motion of the aircraft based on the analysis of coefficients of aerodynamic damping derivatives. Thermophys. Aeromech. 21, 579–588 (2014). https://doi.org/10.1134/S0869864314050060

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  • DOI: https://doi.org/10.1134/S0869864314050060

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