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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2011, Volume 52, Issue 4, Pages 52–62
(Mi pmtf1502)
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This article is cited in 4 scientific papers (total in 4 papers)
Analysis of the reasons for an aerodynamic hysteresis in flight tests of the Soyuz reentry capsule at the hypersonic segment of its descent
O. N. Khatuntseva S. P. Korolev Rocket and Space Corporation "Energia", Korolev, 141070, Russia
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.
Keywords:
hysteresis, damping, aerodynamic coefficients.
Received: 21.04.2010 Accepted: 10.06.2010
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
Linking options:
https://www.mathnet.ru/eng/pmtf1502 https://www.mathnet.ru/eng/pmtf/v52/i4/p52
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Abstract page: | 30 | Full-text PDF : | 8 |
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