Effect of Unsteady Wake Passing Frequency on Boundary Layer Transition, Experimental Investigation, and Wavelet Analysis
Author:
Affiliation:
1. Turbomachinery Performance and Flow Research Laboratory, Texas A&M University, College Station, TX 77843-3123
2. Department of Mechanical and Aerospace Engineering, Syracuse University, Syracuse, NY
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/125/2/251/5902359/251_1.pdf
Reference55 articles.
1. Evans, R. L. , 1978, “Boundary-Layer Development on an Axial-Flow Compressor Stator Blade,” ASME J. Eng. Power, 100, pp. 287–293.
2. Evans, R. L. , 1982, “Boundary Layer Transition and Separation on a Compressor Rotor Airfoil,” ASME J. Eng. Power, 104, pp. 251–253.
3. Walker, G. J., 1974, “The Unsteady Nature of Boundary Layer Transition on an Axial-Flow Compressor Blade,” ASME Paper No. 74-GT-135.
4. Walker, G. J., 1982, “The Turbulent Boundary Layer on an Axial Compressor Blade,” ASME Paper No. 82-GT-52.
5. Walker, G. J. , 1989, “Transitional Flow on Axial Turbomachine Blading,” AIAA J., 27, pp. 595–602.
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