Numerical Investigation of Mach 2.5 Axisymmetric Turbulent Shock Wave Boundary Layer Interactions.

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Bibliographic Details
Title: Numerical Investigation of Mach 2.5 Axisymmetric Turbulent Shock Wave Boundary Layer Interactions.
Authors: Mosele, John-Paul1, jgmosele@nmsu.edu, Gross, Andreas1, Slater, John2
Source: Aerospace (MDPI Publishing); Feb2023, Vol. 10 Issue 2, p159, 30p
Database: Applied Science & Technology Source
Description
ISSN:22264310
DOI:10.3390/aerospace10020159