تعیین محدوده ناپایداری عملکرد و تحلیل اثر گرداب‌های مناطق نوک و ریشه‌ تیغه در یک فن جریان محوری بازگشت‌پذیر

[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