Journals
Publish with us
Publishing partnerships
About us
Blog
Journal of Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
Journal of Engineering
/
2023
/
Article
/
Fig 43
/
Research Article
Analysis of the Shock Wave/Boundary Layer Interaction considering a Compression Corner Model Using the MacCormack Method
Figure 43
Temperature distributions at Mach number 3 and 15 deg (without separation) with the adiabatic wall.