Determination the performance instability range and analysis of the effect of blade tip and hub vortices in a reversible axial flow fan

Document Type : Original Article

Authors

Faculty of Mechanical Engineering, University of Guilan

Abstract

The main goal of the present study is to determine the stable and unstable performance limits of a reversible axial flow fan by 3D numerical simulation. Reversible axial fans are a special type of axial fans that have the ability to create air flow in both directions by using a symmetrical blade profile in them. The main use of these fans is to discharge smoke and polluted air from channels and highway tunnels in emergency situations such as fire and also in normal operating conditions. In the present study, a reversible axial flow fan has been simulated three-dimensionally.The qualitative results obtained from the numerical simulation indicate the presence of instability and the creation of vortices in areas such as the tip of the blade (flow leakage from the pressure surface to the suction in the gap distance of the tip of the blade) and also on the trailing edge and the suction surface of the blades (flow separation) in lower volume flows  from 26 (m3/s) and entering the fan in the stall area. The study of aerodynamic parameters and performance curves shows that the best performance range of the fan at a rotational speed of 900 rpm, is in the volume flow range of more than 26 (m3/s). 

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https://creativecommons.org/licenses/by/4.0/

[1] Spasić Ž, Jovanović M, Bogdanović-Jovanović J. Design and performance of low-pressure reversible axial fan with doubly curved profiles of blades. Journal of Mechanical Science and Technology. 2018;32(8):3707-12.
[2] McKenzie AB. Axial flow fans and compressors. Aerodynamic Design and Performance. 1997.
[3] Keklikoglu H. Design, conctruction and performance evaluation of axial Flow fans 2019.
[4] Bleier FP.  Fan handbook: Selection, application, and design: McGraw-Hill.; 1998.
[5] Moghadam SMA, Meinke M, Schröder W. Analysis of tip-leakage flow in an axial fan at varying tip-gap sizes and operating conditions. Computers & Fluids. 2019;183:107-29.
[6] Lee H, Park K, Choi H. Experimental investigation of tip-leakage flow in an axial flow fan at various flow rates. Journal of Mechanical Science and Technology. 2019;33(3):1271-8.
[7] Benedek T, Vad J, Lendvai B. Combined acoustic and aerodynamic investigation of the effect of inlet geometry on tip leakage flow noise of free-inlet free-exhaust low-speed axial flow fans. Applied Acoustics. 2022;187:108488.
[8] Abdolmaleki M, Mohammadian Bishe E, Afshin H, Farhanieh B. Numerical and experimental study of a reversible axial flow fan. International Journal of Computational Fluid Dynamics. 2020;34(3):173-86.
[9] Wang J, Kruyt NP. Computational fluid dynamics simulations of aerodynamic performance of low-pressure axial fans with small hub-to-tip diameter ratio. Journal of Fluids Engineering. 2020;142(9):091202.
[10] Abdolmaleki M, Afshin H, Farhanieh B. Performance analysis of elliptic-profile airfoil cascade for designing reversible axial flow fans. AIAA Journal. 2019;57(4):1492-501.
[11] Jung JH, Joo W-G. The effect of the entrance hub geometry on the efficiency in an axial flow fan. International Journal of Refrigeration. 2019;101:90-7.
[12] Tóth B, Vad J. Algorithmic localisation of noise sources in the tip region of a low-speed axial flow fan. Journal of Sound and Vibration. 2017;393:425-41.
[13] Luo B, Chu W, Zhang H. Tip leakage flow and aeroacoustics analysis of a low-speed axial fan. Aerospace Science and Technology. 2020;98:105700.
[14] Gullberg P, Sengupta R. Axial fan performance predictions in CFD, comparison of MRF and sliding mesh with experiments. SAE Technical Paper; 2011. Report No.: 0148-7191.
[15] Tian W, Ozbay A, Wang X, Hu H. Experimental investigation on the wake interference among wind turbines sited in atmospheric boundary layer winds. Acta Mechanica Sinica. 2017;33:742-53.
[16] Ghorbanian K, Soltani MR, Manshadi MD. Experimental investigation on turbulence intensity reduction in subsonic wind tunnels. Aerospace science and Technology. 2011;15(2):137-47.
[17] Wilcox DC. Reassessment of the scale-determining equation for advanced turbulence models. AIAA journal. 1988;26(11):1299-310.
[18] Menter FR. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA journal. 1994;32(8):1598-605.
[19] Khoshnejad A, Ebrahimi R, Pouryoussefi SG. Numerical investigation of plasma actuator induced forcing direction on the performance of a low-speed isolated axial compressor rotor. Journal of Electrostatics. 2022;118:103732.
[20] Menter FR, Kuntz M, Langtry R. Ten years of industrial experience with the SST turbulence model. Turbulence, heat and mass transfer. 2003;4(1):625-32.
[21] Anzalotta C, Joshi K, Fernandez E, Bhattacharya S. Effect of forcing the tip-gap of a NACA0065 airfoil using plasma actuators: a proof-of-concept study. Aerospace Science and Technology. 2020;107:106268.
[22] Turton RK. Principles of turbomachinery: Springer Science & Business Media; 2012
  • Receive Date: 22 November 2023
  • Revise Date: 22 January 2024
  • Accept Date: 07 February 2024
  • Publish Date: 28 February 2024