Flow fields with vortex in a small semi-open axial fan
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-009-0294-z.pdf
Reference4 articles.
1. Inoue M., Kuroumaru M., and Furukawa M.: Behavior of Tip Leakage Flow Behind an Axial Compressor Rotor, Trans. ASME, Journal of Engineering for Gas Turbines and Power, Vol. 108, pp.7–14, (1986).
2. Lakshminarayana B., Zaccaria M., and Marathe B.: The Structure of Tip Clearance Flow in Axial Flow Compressors, Trans. ASME, Journal of Turbomachinery, Vol. 117, pp.336–347, (1995).
3. Furukawa M., Inoue M., Saiki K., Yamada M.: The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics, Trans. ASME Journal of Turbomachinery, Vol. 121, pp.469–480, (1999).
4. Fukano T, Fukuhara M., Kawagoe K., Hara Y. and Kinoshita K.: Experimental Study on the Noise Reduction of a Propeller Fan (1st Report, Aerodynamic Characteristics), Trans. JSME, 56–531, B, pp.3378–3382, (1990) (in Japanese).
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