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Flow fields with vortex in a small semi-open axial fan

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Abstract

In order to clarify the effect of tip clearance (TC) size on fan performance and the flow field at rotor outlet in a small semi-open axial fan, the experimental investigation was carried out. The tip diameter of test fan rotor was 180mm and test TC sizes were 1mm (TC=1mm) and 4mm (TC=4mm). Fan characteristics tests were carried out for two cases of TC size and three-dimensional velocity fields at rotor outlet were measured using a single slant hot-wire probe at four flow-rate conditions. As a result, it was found that the pressure — flow-rate characteristics curves for two cases showed almost the same tendency. However, the ensemble averaged velocity profiles along radial measurement stations of TC=4mm largely changed compared with that of TC=1mm in cases of small flow-rate condition. From the phase-locked averaging results, it was also found that the vortex existed in the rotor outlet flow field of high flow-rate condition for each TC case. Compared with the vortices for TC=1mm and TC=4mm, the vortex for TC=4mm was stronger than that for TC=1mm.

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References

  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).

    Article  Google Scholar 

  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).

    Article  Google Scholar 

  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).

    Article  Google Scholar 

  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).

    Google Scholar 

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Shiomi, N., Kinoue, Y., Jin, Y.z. et al. Flow fields with vortex in a small semi-open axial fan. J. Therm. Sci. 18, 294–300 (2009). https://doi.org/10.1007/s11630-009-0294-z

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  • DOI: https://doi.org/10.1007/s11630-009-0294-z

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