Numerical simulation of shock attenuation with real gas effects and a turbulent boundary layer in the expansion tube

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Publication Details

Journal
Shock Waves
Published
2024-10-14
DOI
https://doi.org/10.1007/s00193-024-01198-x
Citations
3
Primary Topic
Computational Fluid Dynamics and Aerodynamics
Type
article
Field-Weighted Citation Impact
1.12

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article

Numerical simulation of shock attenuation with real gas effects and a turbulent boundary layer in the expansion tube

Shintaro Sato, Naofumi Ohnishi, Hiroki Sakamoto
3 citations
Shock Waves
Computational Fluid Dynamics and Aerodynamics
1.12
article

Numerical simulation of shock attenuation with real gas effects and a turbulent boundary layer in the expansion tube

Shintaro Sato, Naofumi Ohnishi, Hiroki Sakamoto
article en
3 citations

Abstract

No abstract available for this paper.
Shock WavesVol. 34(6)
Tohoku University (JP)
Japan Aerospace Exploration Agency
Openalex Percentile: Top 25%
Computational Fluid Dynamics and Aerodynamics
1.12
DOIOpen Access PDFOpenAlex
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Numerical simulation of shock attenuation with real gas effects and a turbulent boundary layer in the expansion tube — Shintaro Sato, Naofumi Ohnishi, et al. · Shock Waves (2024) | TGRS Research Map | TGRS