Investigation of the Calmed Region Behind a Turbulent Spot
Author:
Affiliation:
1. University of Leicester, Leicester, United Kingdom
2. University of Tasmania, Hobart, Tasmania, Australia
3. University of Technology, Sydney, Sydney, Australia
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/119/4/802/5840660/802_1.pdf
Reference19 articles.
1. Blackwelder, R. F., 1993, private communication.
2. Cumpsty, N. A., Dong, Y., and Li, Y. S., 1995, “Compressor Blade Boundary Layers in the Presence of Wakes,” ASME Paper No. 95-GT-443.
3. Gostelow, J. P., Melwani, N., Solomon, W. J., and Walker, G. J., 1995, “Effects of a Self-Similar Adverse Pressure Distribution on Turbulent Spot Development,” AIAA Paper No. 95-2254.
4. Gostelow, J. P., and Hong, G., 1995, “Representation of Boundary Layer Transition and Turbulent Spots in Temporal and Frequency Domains,” Proc. 7th ISFV, Seattle; Flow Visualization VII, Begell House, New York, pp. 218–223.
5. Gostelow J. P. , MelwaniN., and WalkerG. J., 1996, “Effects of Streamwise Pressure Gradient on Turbulent Spot Development,” ASME JOURNAL OF TURBOMACHINERY, Vol. 118, pp. 737–743.
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