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....
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| 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 |
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| Institution: | Nanyang Technological University |
| Summary: | 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. The specific goals of the programme are to: 1. acquire detailed fundamental fluid dynamics for the forced mixer flows 2. establish the important design criteria for the forced mixers. 3. determine the most desirable forced mixer geometry for a wide range of thrust class turbo-fan engines. |
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