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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Bibliographic Details
Main Authors: Yu, Simon Ching Man., Chan, W. K., Chua, L. P.
Other Authors: School of Mechanical and Production Engineering
Format: Research Report
Published: 2008
Subjects:
Online Access:http://hdl.handle.net/10356/6857
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Institution: Nanyang Technological University
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