Email this article Static Hysteresis of the Aerodynamic Characteristics of a Model Aircraft in the Landing Regime
- Authors: Voevodin A.V.1, Soudakov V.G.1
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Affiliations:
- Central Aerohydrodynamic Institute (TsAGI)
- Issue: Vol 53, No 4 (2018)
- Pages: 510-516
- Section: Article
- URL: https://journals.rcsi.science/0015-4628/article/view/155937
- DOI: https://doi.org/10.1134/S0015462818040122
- ID: 155937
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Abstract
Flow past a simplified model of the civil aircraft is numerically investigated in the landing regime. The numerical modeling is performed within the framework of the Reynolds equations. The aerodynamic characteristics of the model are studied. Regimes with the static hysteresis are found.
About the authors
A. V. Voevodin
Central Aerohydrodynamic Institute (TsAGI)
Author for correspondence.
Email: voevodinav@mail.ru
Russian Federation, ul. Zhukovskogo 1, Zhukovsky, Moscow oblast, 140180
V. G. Soudakov
Central Aerohydrodynamic Institute (TsAGI)
Email: voevodinav@mail.ru
Russian Federation, ul. Zhukovskogo 1, Zhukovsky, Moscow oblast, 140180
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