In some cases, the mass flow rate needed to prevent ingress through rim seals in turbine is smaller than that entrained by a free disk. In order to obtain the heat transfer features of the rotor-stator system at such a small mass flow rate, a combined computational and theoretical study has been carried out. It is found that the average Nusselt number (Nuav) on the rotor drops approximately linearly down to zero with decreasing turbulent flow parameter (λt) when λt is smaller than λt,c (λt,c < λt,fd), while Nuav almost keeps constant when λt is larger than λt,c. A correlation between Nuav and λt has been developed, which is expected to be useful in determining disk temperatures in the preliminary design of an internal air cooling system. The Eckert number, which can express the relationship between heat generated by windage and heat conducted through disk, turns out to be an important nondimensional number in describing the heat transfer features of such rotor-stator systems. Moreover, the effect of rotational speed on heat transfer when λt,c<λt<λt,fd has been studied, further identifying the significance of the Eckert number.
Skip Nav Destination
ASME Turbo Expo 2012: Turbine Technical Conference and Exposition
June 11–15, 2012
Copenhagen, Denmark
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4470-0
PROCEEDINGS PAPER
Heat Transfer Characteristics of a Rotor-Stator System With Small Radial Outflow
Hongde Jiang,
Hongde Jiang
Tsinghua University, Beijing, China
Search for other works by this author on:
Peter Childs
Peter Childs
Imperial College, London, UK
Search for other works by this author on:
Li Lin
Tsinghua University, Beijing, China
Jing Ren
Tsinghua University, Beijing, China
Hongde Jiang
Tsinghua University, Beijing, China
Peter Childs
Imperial College, London, UK
Paper No:
GT2012-69759, pp. 2283-2293; 11 pages
Published Online:
July 9, 2013
Citation
Lin, L, Ren, J, Jiang, H, & Childs, P. "Heat Transfer Characteristics of a Rotor-Stator System With Small Radial Outflow." Proceedings of the ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. Volume 4: Heat Transfer, Parts A and B. Copenhagen, Denmark. June 11–15, 2012. pp. 2283-2293. ASME. https://doi.org/10.1115/GT2012-69759
Download citation file:
16
Views
0
Citations
Related Proceedings Papers
Related Articles
Influence of Fluid Dynamics on Heat Transfer in a Preswirl Rotating-Disk System
J. Eng. Gas Turbines Power (October,2005)
Heat Transfer in an Air-Cooled Rotor–Stator System
J. Turbomach (July,1996)
Influence of Stator-Rotor Interaction on the Aerothermal Performance of Recess Blade Tips
J. Turbomach (January,2011)
Related Chapters
Introduction
Turbine Aerodynamics: Axial-Flow and Radial-Flow Turbine Design and Analysis
Outlook
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Threshold Functions
Closed-Cycle Gas Turbines: Operating Experience and Future Potential