An unsteady pseudoshock model for barotropic gas flow
- 作者: Lipatov I.I.1, Liapidevskii V.Y.2,3, Chesnokov A.A.2,3
-
隶属关系:
- Zhukovskii Central Institute of Aerohydrodynamics
- Lavrent’ev Institute of Hydrodynamics, Siberian Branch
- Novosibirsk State University
- 期: 卷 61, 编号 2 (2016)
- 页面: 82-86
- 栏目: Mechanics
- URL: https://journals.rcsi.science/1028-3358/article/view/190972
- DOI: https://doi.org/10.1134/S1028335816020075
- ID: 190972
如何引用文章
详细
A mathematical unsteady pseudoshock model describing the continuous transition from supersonic to subsonic flow is constructed for a barotropic gas flow in a long flat channel or a nozzle. The model is based on a two-layer scheme of flow with mass transfer including a potential supersonic core and a turbulent boundary layer.
作者简介
I. Lipatov
Zhukovskii Central Institute of Aerohydrodynamics
Email: chesnokov@hydro.nsc.ru
俄罗斯联邦, Zhukovskii, Moscow oblast, 140160
V. Liapidevskii
Lavrent’ev Institute of Hydrodynamics, Siberian Branch; Novosibirsk State University
Email: chesnokov@hydro.nsc.ru
俄罗斯联邦, Novosibirsk, 630090; Novosibirsk, 630090
A. Chesnokov
Lavrent’ev Institute of Hydrodynamics, Siberian Branch; Novosibirsk State University
编辑信件的主要联系方式.
Email: chesnokov@hydro.nsc.ru
俄罗斯联邦, Novosibirsk, 630090; Novosibirsk, 630090
补充文件
