Investigation of Three-Dimensional Unsteady Flows in a Two-Stage Shrouded Axial Turbine Using Stereoscopic PIV—Kinematics of Shroud Cavity Flow
Author:
Affiliation:
1. School of Mechanical and Aerospace Engineering, Seoul National University, Seoul 151-742, Korea
2. Turbomachinery Laboratory, Swiss Federal Institute of Technology Zurich, Zurich CH-8092, Switzerland
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2720873/5582865/011021_1.pdf
Reference24 articles.
1. Loss Mechanisms in Turbomachines—The 1993 IGTI Scholar Lecture;Denton;ASME J. Turbomach.
2. Hunter, S. D., and Manwaring, S. R., 2000, “Endwall Cavity Flow Effects on Gaspath Aerodynamics in an Axial Flow Turbine—Part I: Experimental and Numerical Investigation,” ASME Paper No. 2001-GT-651.
3. The Control of Shroud Leakage Flows to Reduce Aerodynamic Losses in a Low Aspect Ratio, Shrouded Axial Flow Turbine;Wallis;ASME J. Turbomach.
4. Peters, P., Breisig, V., Giboni, A., Lerner, C., and Pfost, H., 2000, “The Influence of the Clearance of Shrouded Rotor Blades on the Development of the Flowfield and Losses in the Subsequent Stator,” ASME Paper No. 2000-GT-478.
5. Giboni, A., Menter, J. R., Peters, P., Wolter, K., Pfost, H., and Breisig, V., 2003, “Interaction of Labyrinth Seal Leakage Flow and Main Flow in an Axial Turbine,” ASME Paper No. GT2003-38722.
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