Boundary Layer Development in Axial Compressors and Turbines: Part 2 of 4—Compressors
Author:
Affiliation:
1. GE Aircraft Engines, Cincinnati, OH 45215
2. Iowa State University, Ames, IA 50011
3. University of Tasmania, Hobart, Tasmania
4. University of Cambridge, Cambridge, United Kingdom
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/119/3/426/5631730/426_1.pdf
Reference5 articles.
1. McFarland, V. E., and Tiderman, W. G., 1992, “Viscous Interaction Upstream and Downstream of a Turbine Stator Cascade With a Periodic Wake Effect,” ASME Paper No. 92-GT-162.
2. O’Brien J. E. , and CappS. P., 1989, “Two-Component Phase-Averaged Turbulence Statistics Downstream of a Rotating Spoked-Wheel Wake Generator,” ASME JOURNAL OF TURBOMACHINERY, Vol. 111, pp. 475–482.
3. Orth U. , 1993, “Unsteady Boundary Layer Transition in Flow Periodically Disturbed by Wakes,” ASME JOURNAL OF TURBOMACHINERY, Vol. 15, pp. 707–713.
4. Pfeil, H., and Herbst, R., 1979, “Transition Procedure of Instationary Boundary Layers,” ASME Paper No. 79-GT-128.
5. Wittig, S., Schulz, A. Dullenkopf, K., and Fairbank, J., 1988, “Effects of Free-Stream Turbulence and Wake Characteristics on the Heat Transfer Along a Cooled Gas Turbine Blade,” ASME Paper No. 88-GT-179.
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