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Design of Sinusoidal Leading Edge for Low-Speed Axial Fans Operating under Inflow Distortion

Author

Listed:
  • Lorenzo Tieghi

    (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Via Eudossiana 18, 00182 Rome, Italy)

  • Giovanni Delibra

    (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Via Eudossiana 18, 00182 Rome, Italy)

  • Johan Van der Spuy

    (Department of Mechanical and Mechatronic Engineering, Stellenbosh University, Stellenbosch Central, Stellenbosh 7599, South Africa)

  • Alessandro Corsini

    (Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Via Eudossiana 18, 00182 Rome, Italy)

Abstract

Axial fans may be equipped with passive flow control devices to enhance rotor efficiency or minimize noise emissions. In this regard, blade designs influenced by biomimicry, such as rotors with sinusoidal leading edges (LEs), have gained popularity in recent years. However, their design is predominantly driven by a trial-and-error approach, with limited systematic studies on the influence of rotor performance. Furthermore, their effectiveness is typically evaluated under controlled conditions that may significantly differ from operations in real installation layouts. In this work, a systematic review of the design process for sinusoidal LE axial fan rotors is provided, aiming to summarize previous design experiences. Then, a modified sinusoidal LE is designed and fitted to a 7.3 m low-speed axial fan for air-cooled condensers (ACCs). These fans operate at environmental conditions, providing a quasi-zero static pressure rise, often with inflow non-uniformities. A series of RANS computations were run to simulate the performance of the baseline fan and that of the sinusoidal leading edge, considering a real installation setup at Stellenbosh University, where the ACC is constrained between buildings and has a channel running on the ground below the fan inlet. The aim is to explore the nonbalanced inflow condition effects in both rotor geometries and to test the effect of the installation layout on fan performance. The results show that the modification to the rotor allows for a more even distribution of flow in the blade-to-blade passages with respect to the baseline geometry.

Suggested Citation

  • Lorenzo Tieghi & Giovanni Delibra & Johan Van der Spuy & Alessandro Corsini, 2024. "Design of Sinusoidal Leading Edge for Low-Speed Axial Fans Operating under Inflow Distortion," Energies, MDPI, vol. 17(5), pages 1-17, February.
    • Handle: RePEc:gam:jeners:v:17:y:2024:i:5:p:1150-:d:1347889
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    References listed on IDEAS

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    1. Chen, Lei & Yang, Lijun & Du, Xiaoze & Yang, Yongping, 2016. "A novel layout of air-cooled condensers to improve thermo-flow performances," Applied Energy, Elsevier, vol. 165(C), pages 244-259.
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