Inter-turbine diffusers offer the potential advantage of reducing the flow coefficient in the following stages leading to increased efficiency. The flows associated with these ducts differ from those in simple annular diffusers both as a consequence of their high-curvature S-shaped geometry and of the presence of wakes created by the upstream turbine. Experimental data and numerical simulations clearly reveal the generation of significant secondary flows as the flow develops through the diffuser in the presence of cross-passage pressure gradients. The further influence of inlet swirl is also demonstrated. Data from experimental measurements with and without an upstream turbine are discussed and computational simulations are shown not only to give a good prediction of the flow development within the diffuser but also to demonstrate the importance of modelling the fully three-dimensional nature of the flow.
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ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition
June 10–13, 1996
Birmingham, UK
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7872-9
PROCEEDINGS PAPER
Flow Development Through Inter-Turbine Diffusers
Robert G. Dominy,
Robert G. Dominy
University of Durham, Durham, UK
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David A. Kirkham,
David A. Kirkham
University of Durham, Durham, UK
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Andrew D. Smith
Andrew D. Smith
Rolls-Royce PLC, Derby, UK
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Robert G. Dominy
University of Durham, Durham, UK
David A. Kirkham
University of Durham, Durham, UK
Andrew D. Smith
Rolls-Royce PLC, Derby, UK
Paper No:
96-GT-139, V001T01A044; 7 pages
Published Online:
February 6, 2015
Citation
Dominy, RG, Kirkham, DA, & Smith, AD. "Flow Development Through Inter-Turbine Diffusers." Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 1: Turbomachinery. Birmingham, UK. June 10–13, 1996. V001T01A044. ASME. https://doi.org/10.1115/96-GT-139
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