A supersonic viscous gas flow past a blunt cylindrical body bounded at its ends by parallel plates

The paper presents the results of calculations of a supersonic laminar flow past a cylindrical body located between parallel horizontal walls (plates). The free-stream Mach number M = 5. Calculations were carried out for various values of the geometric factor χ defined as the ratio of the distance b...

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Bibliographic Details
Main Authors: Kolesnik Elizaveta, Babich Elena, Smirnov Evgeny
Format: Article
Language:English
Published: Peter the Great St.Petersburg Polytechnic University 2025-03-01
Series:St. Petersburg Polytechnical University Journal: Physics and Mathematics
Subjects:
Online Access:https://physmath.spbstu.ru/article/2025.78.02/
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