View in EDS

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

Saved in:
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
Be the first to leave a comment!
You must be logged in first