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.
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Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 52, No. 4, pp. 52–62, July–August, 2011.
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Khatuntseva, O.N. 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 Tech Phy 52, 544–552 (2011). https://doi.org/10.1134/S0021894411040067
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DOI: https://doi.org/10.1134/S0021894411040067