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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| Online Access: | http://hdl.handle.net/10356/6857 |
| _version_ | 1826112690708283392 |
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| author | Yu, Simon Ching Man. Chan, W. K. Chua, L. P. |
| author2 | School of Mechanical and Production Engineering |
| author_facet | School of Mechanical and Production Engineering Yu, Simon Ching Man. Chan, W. K. Chua, L. P. |
| author_sort | Yu, Simon Ching Man. |
| collection | NTU |
| description | 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. |
| first_indexed | 2024-10-01T03:10:53Z |
| format | Research Report |
| id | ntu-10356/6857 |
| institution | Nanyang Technological University |
| last_indexed | 2024-10-01T03:10:53Z |
| publishDate | 2008 |
| record_format | dspace |
| spelling | ntu-10356/68572023-03-04T18:06:25Z Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer Yu, Simon Ching Man. Chan, W. K. Chua, L. P. School of Mechanical and Production Engineering DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines 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. 2008-09-17T14:35:50Z 2008-09-17T14:35:50Z 2005 2005 Research Report http://hdl.handle.net/10356/6857 Nanyang Technological University application/pdf |
| spellingShingle | DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines Yu, Simon Ching Man. Chan, W. K. Chua, L. P. Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title | Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title_full | Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title_fullStr | Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title_full_unstemmed | Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title_short | Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer |
| title_sort | advanced aerospace research on the new generation of turbo fan engine exhaust mixer |
| topic | DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines |
| url | http://hdl.handle.net/10356/6857 |
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