Numerical Investigation of Asymmetric Mach 2.5 Turbulent Shock Wave Boundary Layer Interaction.
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| Title: | Numerical Investigation of Asymmetric Mach 2.5 Turbulent Shock Wave Boundary Layer Interaction. |
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| Authors: | Mosele, John-Paul1, jgmosele@nmsu.edu, Gross, Andreas1, Slater, John2 |
| Source: | Aerospace (MDPI Publishing); May2023, Vol. 10 Issue 5, p417, 29p |
| Database: | Applied Science & Technology Source |
| ISSN: | 22264310 |
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| DOI: | 10.3390/aerospace10050417 |
