电邮这篇文章 Static Hysteresis of the Aerodynamic Characteristics of a Model Aircraft in the Landing Regime
- 作者: Voevodin A.V.1, Soudakov V.G.1
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隶属关系:
- Central Aerohydrodynamic Institute (TsAGI)
- 期: 卷 53, 编号 4 (2018)
- 页面: 510-516
- 栏目: Article
- URL: https://journals.rcsi.science/0015-4628/article/view/155937
- DOI: https://doi.org/10.1134/S0015462818040122
- ID: 155937
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详细
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.
作者简介
A. Voevodin
Central Aerohydrodynamic Institute (TsAGI)
编辑信件的主要联系方式.
Email: voevodinav@mail.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, Moscow oblast, 140180
V. Soudakov
Central Aerohydrodynamic Institute (TsAGI)
Email: voevodinav@mail.ru
俄罗斯联邦, ul. Zhukovskogo 1, Zhukovsky, Moscow oblast, 140180
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