Control of Shroud Leakage Loss by Reducing Circumferential Mixing
Author:
Affiliation:
1. Whittle Laboratory, Cambridge University, Cambridge, CB30DY, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2750682/5680283/021010_1.pdf
Reference11 articles.
1. Wallis, A. M., Denton, J. D., and Demargne, A. A. J., 2000, “The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine,” ASME Paper No. 2000-GT-475.
2. Denton, J. D., and Johnson, C. G., 1976, “An Experimental Study of the Tip Leakage Flow Around Shrouded Turbine Blades,” CEGB Report No. R/M/N848, Marchwood Engineering Laboratories, UK.
3. Giboni, A., Wolter, K., Menter, J. R. P., and Pfost, H., 2004, “Experimental and Numerical Investigation Into the Unsteady Interaction of Labyrinth Seal Leakage Flow and Main Flow in a 1.5 Stage Axial Turbine,” ASME Paper No. GT2004-53024.
4. Peters, P., Menter, J. R., Pfost, H., Giboni, A., and Wolter, K., 2005, “Unsteady Interaction of Labyrinth Seal Leakage Flow and Downstream Stator Flow in a Shrouded 1.5 Stage Axial Turbine,” ASME Paper No. GT2005-68065.
5. Pfau, A., Kalfas, A. I., and Abhari, R. S., 2004, “Making Use of Labyrinth Interaction Flow,” ASME Paper No. GT2004-53797.
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