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Numerical Investigation of Asymmetric Mach 2.5 Turbulent Shock Wave Boundary Layer Interaction.

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Bibliographic Details
Title: Numerical Investigation of Asymmetric Mach 2.5 Turbulent Shock Wave Boundary Layer Interaction.
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
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