Flow Instability Within a Diffusing, Annular S-Shaped Duct
Author:
Affiliation:
1. Frazer-Nash Consultancy Ltd., Bristol, United Kingdom
2. University of Durham, Durham, United Kingdom
3. Rolls-Royce PLC, Derby, United Kingdom
Abstract
Publisher
American Society of Mechanical Engineers
Link
http://asmedigitalcollection.asme.org/GT/proceedings-pdf/doi/10.1115/99-GT-070/4215566/v001t03a009-99-gt-070.pdf
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. The Effect of Rotor Tip Clearance Size onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage;Journal of Turbomachinery;2012-05-11
2. Research on the aerodynamics of intermediate turbine diffusers;Progress in Aerospace Sciences;2011-05
3. Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept;Journal of Turbomachinery;2009-07-06
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