Design of heated flow wind tunnel facility for testing small size ramjet engine combustors
This report documents the research studies on the design of a 'high speed heated flow wind tunnel facility', to test a 'Trapped Vortex Concept' (TVC) combustor of a ramjet engine, designed for the DSO National Laboratories, Singapore. The ramjet is to operate at flight s...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Theses and Dissertations |
| Language: | English |
| Published: |
2015
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/65089 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |
Be the first to leave a comment!