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Open Accesshttps://doi.org/10.18372/2306-1472.23.1112
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Cite Publication Date: Jan 1, 2005 | |
 License type: cc-by-nc-nd |
Flow of viscous compressible gas is considered in the airfoil cascade of the thin plates with great negative angle of attack. Influence of wall boundary layer upon a mode of flow choking in the airfoil cascade is estimated in the article.
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