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Original Articles

Numerical investigation of blade tip with different groove effect and its dynamic analysis of axial flow fan

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Pages 1785-1793 | Received 25 Mar 2019, Accepted 01 May 2019, Published online: 31 May 2019

References

  • Beheshti, Behnam H., Joao A. Teixeira, Paul C. Ivey, Kaveh Ghorbanian, and Bijan Farhanieh. 2015. “Parametric Study of Tip Clearance- Casing Treatment on Performance and Stability of a Transonic Axial Compressor.” Energy 82: 556–569. doi: https://doi.org/10.1016/j.energy.2015.01.065
  • Corsini, A., F. Rispoli, and A. G. Shreard. 2007. “Development of Improved blade Tip Endplate Concepts for Low-noise Operation in Industrial Fans.” Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 221: 669–681.
  • Dinh, Cong-Truong, Man-Woong Heo, and Kwang-Yong Kim. 2015. “Aerodynamic Performance of Transonic Axial Compressor with a Casing Groove Combined with Blade Tip Injection and Ejection.” Aerospace Science and Technology 46: 176–187. doi: https://doi.org/10.1016/j.ast.2015.07.006
  • Huang, Cheng-Hung, and Chung-Wei Gau. 2012. “An Optimal Design for Axialflow Fan Blade: Theoretical and Experimental Studies.” Journal of Mechanical Science and Technology 26 (2): 427–443. doi: https://doi.org/10.1007/s12206-011-1030-7
  • Kameier, F., and W. Neise. 1997. Experimental Study of Tip Clearance Losses and Noise in Axial Turbomachines and their Reduction.” J Turbomach 119 (3): 460–471. doi: https://doi.org/10.1115/1.2841145
  • Müller, Martin W., and Heinz-Peter Schiffer. 1997. “Effect of Circumferential Grooves on the Aerodynamic Performance of an AxialSingle-stage Transonic Compressor.” ASME Turbo Expo 2007: Power for Land, Sea, and Air Volume 6: Turbo Expo 2007, Parts A and B, Montreal, Canada, May 14–17, 2007.
  • Nho, Young Cheol, Jung Shin Park, Yong Jin Lee, and Jae Su Kwak. 2012. “Effects of Turbine Blade Tip Shape on Total Pressure Loss and Secondary Flow of a Linear Turbine Cascade.” International Journal of Heat and Fluid Flow 33 (1): 92–100. doi: https://doi.org/10.1016/j.ijheatfluidflow.2011.12.002
  • Panchal, Hitesh, and Nikunj Patel. 2018. “ANSYS CFD and Experimental Comparison of Various Parameters of a Solar Still.” International Journal of Ambient Energy 39 (6): 551–557. doi: https://doi.org/10.1080/01430750.2017.1318785
  • Shezencity, Minj Juchen. “Axial Flow Fan blade structure and Axial flow fan”.
  • Thompson, D. W., P. I. King, and D. C. Rabe. 1998. “Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-flow Compressor Rotor.” J Turbomach 120 (3): 477–486. doi: https://doi.org/10.1115/1.2841743
  • Ye, Xuemin, Pengmin Li, Chunxi Li, and Xueliang Ding. 2015. “Numerical Investigation of Blade Tip Grooving Effect on Performance and Dynamics of an Axial Flow Fan.” Energy 82: 556–569. doi: https://doi.org/10.1016/j.energy.2015.01.065
  • Yuan, S. Q., J. F. Zhang, J. P. Yuan, Y. S. He, and Y. D. Fu. 2006. “Analysis of the Influence of Splitter Blade Centrifugal Pump Impeller Flow.” Symp CSAM, 209e14. [in Chinese].
  • Zhang, Z. X. 2012, April. “Aerodynamic Performance and Vibration Characteristics Study for Horizontal Axis Wind Turbine Blade.” Master Dissertation. College of mechanical Engineering. Zhejiang University of Technology [in Chinese, Hangzhou, Zhejiang].

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