SUPERSONIC VISCOUS FLOW PAST THE JUNCTION OF A PLATE AND A CYLINDRICAL BODY: NUMERICAL SOLUTION FOR MACH NUMBER OF 2.95
Results of numerical simulation of shock-wave pattern and vortex structures forming in supersonic flow past a cylindrical body, which penetrates the approaching flat-plate boundary layer up to the plate, are presented. The laminar flow case with Mach number of 2.95 is considered. Comparison of numer...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Peter the Great St.Petersburg Polytechnic University
2019-06-01
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| Series: | St. Petersburg Polytechnical University Journal: Physics and Mathematics |
| Subjects: | |
| Online Access: | https://physmath.spbstu.ru/article/2019.44.01/ |