Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer
The objectives of this research program are: (a) to establish and to enhance the R&D capability in Aerospace Technology with particular reference to the turbo-fan engine exhausts. (b) to develop a forced mixer geometry that can be used for a wide range of thrust class turbo-fan engine exhausts....
| Main Authors: | , , |
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| Other Authors: | |
| Format: | Research Report |
| Published: |
2008
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| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/6857 |