Influence of Flow Coefficient, Stagger Angle, and Tip Clearance on Tip Vortex in Axial Compressors
Author:
Affiliation:
1. School of Mechanical and Aerospace Engineering, Seoul National University, San 56-1, Shillim dong, Kwanak gu, Seoul, 151-744, Korea
2. GE Transportation, Aircraft Engines, 1 Neumann Way, Cincinnati, Ohio, 45215
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/128/6/1274/5834905/1274_1.pdf
Reference21 articles.
1. Rains, D. A. , 1954, “Tip Clearance Flow in Axial Flow Compressors and Pumps,” Hydrodynamics and Mechanical Engineering Laboratories Report, No. 5.
2. Endwall Blockage in Axial Compressors;Khalid;ASME J. Turbomach.
3. An Approximate Analysis and Prediction Method for Tip Clearance Loss in Axial Compressors;Storer;ASME J. Turbomach.
4. Tip Clearance Flow in a Compressor Rotor Passage at Design and Off-Design Conditions;Lakshminarayana;ASME J. Eng. Gas Turbines Power
5. Martinez-Sanchez, M., and Gauthier, R. P., 1990, “Blade Scale Effects of Tip Leakage,” Gas Turbine Laboratory Report #202, M.I.T.
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