Effects of a kind of non-smooth blade on the unsteady flow field at the exit of an axial fan
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-008-0001-5.pdf
Reference5 articles.
1. Bechert, D.W., Bruse, M. and Hage, W., Experiments with three-dimensional riblets as an idealized model of shark skin, Experiments in Fluids, 2000, Vol.28, pp.403–412.
2. Boese, M., and Fottner, L., Effects of Riblets on the Loss Behavior of a Highly Loaded Compressor Cascade, ASME TURBO EXPO, 2002-GT-30438, Amsterdam, Netherlands, June 2002.
3. Ninnemann, Todd and Wing, F. Ng, Loss Reduction Using Riblets on a Supersonic Through-Flow Fan Blade Cascade, ASME Journal of Fluids Engineering, Vol. 126, July 2004, pp.642–649.
4. Ma, Hongwei, Yan, Wuying, and Tian, Qiao, Influences of a Kind of Groove-blade on the Flow Field in a Compressor Cascade, Journal of Thermal Science, Vol. 15, No. 3, pp. 193–199, 2006.
5. Ma, Hongwei, Guo, Jibo, Effects of a Kind of Non-smooth Blade on the Performance of an Axial Fan, Journal of Thermal Science, Vol. 15, No. 3, pp. 200–205, 2006.
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