Advanced aerospace research on the new generation of turbo-fan engine exhaust mixer

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: Yu, Simon Ching Man., Chan, W. K., Chua, L. P.
Other Authors: School of Mechanical and Production Engineering
Format: Research Report
Published: 2008
Subjects:
DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines
Online Access:http://hdl.handle.net/10356/6857
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Institution: Nanyang Technological University
id sg-ntu-dr.10356-6857
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spelling sg-ntu-dr.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
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
topic DRNTU::Engineering::Aeronautical engineering::Aircraft motors and engines
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
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.
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.
format Research Report
author Yu, Simon Ching Man.
Chan, W. K.
Chua, L. P.
author_sort Yu, Simon Ching Man.
title 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_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_sort advanced aerospace research on the new generation of turbo-fan engine exhaust mixer
publishDate 2008
url http://hdl.handle.net/10356/6857
_version_ 1759853708051480576

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