Abstract:
With the use of a mathematical model developed for describing hysteresis functions of aerodynamic forces and moments depending both on the angle of attack and on the rate of its variation, the emergence of a hysteresis in flight tests of the Soyuz reentry capsule at the hypersonic segment of its descent is found to be induced by damping.
Citation:
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”, Prikl. Mekh. Tekh. Fiz., 52:4 (2011), 52–62; J. Appl. Mech. Tech. Phys., 52:4 (2011), 544–552
\Bibitem{Kha11}
\by O.~N.~Khatuntseva
\paper Analysis of the reasons for an aerodynamic hysteresis in flight tests of the Soyuz reentry capsule at the hypersonic segment of its descent
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2011
\vol 52
\issue 4
\pages 52--62
\mathnet{http://mi.mathnet.ru/pmtf1502}
\elib{https://elibrary.ru/item.asp?id=16973560}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2011
\vol 52
\issue 4
\pages 544--552
\crossref{https://doi.org/10.1134/S0021894411040067}
Linking options:
https://www.mathnet.ru/eng/pmtf1502
https://www.mathnet.ru/eng/pmtf/v52/i4/p52
This publication is cited in the following 5 articles:
M. E. Semenov, A. V. Tolkachev, O. I. Kanishcheva, “A simple mechanical model of turbulence”, Vestnik of Samara University. Natural Science Series, 30:3 (2024), 63
Wanxin Zhang, Jihong Zhu, “Online identification of aerodynamics with fast time‐varying features using Kalman filter”, IET Control Theory & Appl, 15:2 (2021), 272
Wanxin Zhang, Minghua Xia, Jihong Zhu, “LPV Modeling and Identification of Unsteady Aerodynamics for Fast Maneuvering Aircrafts”, IEEE Access, 7 (2019), 92436
M. Rizwanur Rahman, A.B.M. Toufique Hasan, M. Itmam Labib, “Numerical Investigation of Aerodynamic Hysteresis for Transonic Flow Over a Supercritical Airfoil”, Procedia Engineering, 105 (2015), 368
A. A. Dyadkin, O. N. Khatuntseva, “Method determining the nature of oscillating motion of the aircraft based on the analysis of coefficients of aerodynamic damping derivatives”, Thermophys. Aeromech., 21:5 (2014), 579