Journals
Publish with us
Publishing partnerships
About us
Blog
International Journal of Aerospace Engineering
Journal overview
For authors
For reviewers
For editors
Table of Contents
Special Issues
International Journal of Aerospace Engineering
/
2021
/
Article
/
Tab 5
/
Research Article
Comparative Assessment of Modified
-
Models for Scramjet Intake Flow Analysis
Table 5
Grid information of the grid dependency test for the SWL scramjet intake case.
Grid type
Number of cells
Number of grids along the streamwise direction
Number of grids along the transverse direction
Max
Average
Finest
178,000
891 (
)
201
2.51
0.326
Fine
120,000
751 (
)
161
5.62
0.82
Medium
100,800
631 (
)
161
5.63
0.858
Coarse
70,000
501 (
141
8.4
2.27