Improvising the Tesla Micro-Turbine: Experimental and Performance Analysis

Authors

  • Muhammad Nor Ikmal Muhamad Nazri Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Adi Azriff Basri Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Mohd Na'im Abdullah Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Faizal Mustapha Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Farid Bajuri Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Ernnie Illyani Basri Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia
  • Masaaki Tamagawa Graduate School of Life Science and Systems Engineering Department of Biological Functions Engineering, Kyushu Institute of Technology, Fukuoka, Japan

DOI:

https://doi.org/10.37934/arfmts.129.1.5868

Keywords:

Tesla turbine, bladeless micro-turbine, improvisation of tesla turbine, tesla turbine power generation

Abstract

Present Tesla turbine presented a distinct approach to conventional turbine technology by utilizing frictional and viscous forces acting on stacked discs, deviating from the traditional use of blades. Characterized by its efficient energy extraction through boundary layer adhesion and cohesion, the Tesla turbine can achieve exceptional rotational speeds. However, its limited torque output remains a significant challenge, particularly for applications demanding high torque. Hence, the objective of this manuscript is to improvise the design of the Tesla turbine and analyze the impact of the new design’s rotational speed, voltage, current and electrical power generation with increasing inlet pressure. The research methodology employed in this study involves the design of the Tesla turbine discs, then proceeded with experimental work from fabrication of the designed discs and conducting performance tests. It aims to gather quantitative data through controlled experiments to assess the best design of the turbine and test the performance and feasibility of the improvised Tesla turbine. The model comprises of bladed design around the disc performed the best at producing electrical power up to 19.08 W at 50 psi inlet pressure.

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Author Biographies

Muhammad Nor Ikmal Muhamad Nazri, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

ikmalnazri2000@gmail.com

Adi Azriff Basri, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

adiazriff@upm.edu.my

Mohd Na'im Abdullah, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

naimabdullah@upm.edu.my

Faizal Mustapha, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

faizalms@upm.edu.my

Farid Bajuri, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

fari.bajuri@gmail.com

Ernnie Illyani Basri, Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, 43400, Serdang, Selangor, Malaysia

ernebasri@gmail.com

Masaaki Tamagawa, Graduate School of Life Science and Systems Engineering Department of Biological Functions Engineering, Kyushu Institute of Technology, Fukuoka, Japan

tama@life.kyutech.ac.jp

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Published

2025-03-30

How to Cite

Muhamad Nazri, M. N. I., Basri, A. A., Abdullah, M. N., Mustapha, F., Bajuri, F., Basri, E. I., & Tamagawa, M. (2025). Improvising the Tesla Micro-Turbine: Experimental and Performance Analysis. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 129(1), 58–68. https://doi.org/10.37934/arfmts.129.1.5868

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