Analysis of Supersonic Free Jets and Impinging Supersonic Jets on Deflector
<p id="p1">The computational fluid dynamics analysis is carried out to analyze the shock and flow characteristics of under- and over expanded supersonic free jets emanating from convergent-divergent nozzles. Influence of exit Mach number on shock cell lengths are analyzed with the help of density co...
Saved in:
| Main Author: | |
|---|---|
| Format: | Book Chapter |
| Language: | English |
| Published: |
IntechOpen
2023
|
| Subjects: | |
| Online Access: | https://www.intechopen.com/chapters/1158370 |
| Tags: |
No Tags, Be the first to tag this record!
|