Effect of turbine inlet temperature on rotor blade tip leakage flow and heat transfer
Author:
Publisher
Emerald
Subject
Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials
Reference10 articles.
1. An, B.T., Liu, J.‐J. and Jiang, H.‐D. (2008), “Numerical investigation of unsteady effects of hot streak on flow and heat transfer in a turbine stage”,Proceedings of ASME Turbo Expo, Berlin, Germany, GT2008‐50415.
2. An Investigation on Turbine Tip and Shroud Heat Transfer
3. He, L., Menshikova, V. and Haller, B.R. (2004), “Influence of hot streak circumferential length‐scale in transonic turbine stage”,Proceedings of ASME Turbo Expo, Vienna, Austria, GT2004‐53370.
4. Krishnababu, S.K., Newton, P.J., Dawes, W.N., Lock, G.D., Hodson, H.P., Hannis, J. and Whitney, C. (2007), “Aero‐thermal investigations of tip leakage flow in axial flow turbines part I: effect of tip geometry and tip clearance gap”,Proceedings of ASME Turbo Expo, Montreal, Canada, GT2007‐27954.
5. Unsteady Numerical Investigation of Blade Tip Leakage, Part 1: Time-Averaged Results
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