An unsteady pseudoshock model for barotropic gas flow


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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

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