The Influence of Fan Root Flow on the Aerodynamic of a Low-Pressure Compressor Transition Duct
Author:
Affiliation:
1. Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough, Leicestershire LE11 3TU, UK
2. Rolls-Royce Plc., PO Box 31, Derby DE24 8BJ, UK
Abstract
Funder
Loughborough University
Rolls-Royce University Technology Centre
Aerospace Technology Institute
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4045272/6464411/turbo_142_1_011002.pdf
Reference19 articles.
1. Britchford, K. M. , 1998, “The Aerodynamic Behaviour of an Annular S-Shaped Duct,” Ph.D. thesis, Loughborough University, Loughborough.
2. Bailey, D. W. , 1997, “The Aerodynamic Performance of an Annular S-Shaped Duct,” Ph.D. Thesis, Loughborough University, Loughborough.
3. Measurements and Prediction of Flow in Annular S-Shaped Ducts;Britchford,1993
4. The Development of the Mean Flow and Turbulence Structure in an Annular S-Shaped Duct;Britchford,1994
5. The Effect of Operating Conditions on the Aerodynamic Performance of an Integrated OGV S-Shaped Duct;Britchford,2001
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