#TITLE_ALTERNATIVE#
In transonic flow condition, the shock wave boundary layer interaction(SWBLI) and flow separation on wing upper surface of a civil aircraft induce transonic drag divergence. The transonic flow in case of a large drag caused by wave drag. The cause of wave drag are the strong shocks developing on the...
Saved in:
| Main Author: | |
|---|---|
| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/15955 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |