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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2021
/
Article
/
Tab 2
/
Research Article
Comparative Assessment of Modified
-
Models for Scramjet Intake Flow Analysis
Table 2
Grid information of the grid dependency test for the double ramp case.
Grid type
Number of cells
Number of grids in the streamwise direction
Number of grids in the transverse direction
Max
Average
Finest
264,000
661 (
)
401
1.291
0.418
Fine
221,400
616 (
)
361
1.291
0.42
Medium
162,000
541 (
)
301
2.106
0.792
Coarse
104,500
419 (
)
251
5.703
3.139