Aerodynamic performance evaluation of multi inner blades savonius rotor
Savonius wind turbine is the cheapest and simplest type of vertical axis wind turbines. This turbine is being utilized in various countries due to the simplistic design and low construction cost. However, this turbine suffers from low efficiency. For that, this study aims to increase the perfo...
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2020
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my-uthm-ep.9122021-09-09T02:46:39Z Aerodynamic performance evaluation of multi inner blades savonius rotor 2020-09 Al-Ghriybah, Mohanad TL500-777 Aeronautics. Aeronautical engineering Savonius wind turbine is the cheapest and simplest type of vertical axis wind turbines. This turbine is being utilized in various countries due to the simplistic design and low construction cost. However, this turbine suffers from low efficiency. For that, this study aims to increase the performance of the Savonius wind rotor in order to generate more useful power. In the present study, the aerodynamics performance of the Savonius wind turbine rotor with inner blades was investigated. The effect of number of inner blades, angle of inner blades, position of inner blades, and distance between the inner blades were evaluated under low and normal ranges of Tip Speed Ratio (TSR) through simulation and experimental work. A numerical investigation was adopted using ANSYS Fluent 19.1 software in order to determine the aerodynamic performance such as power coefficient (Cp) and torque coefficient (Ct). The numerical investigation was performed using two and three-dimensional simulations based on k-Ɛ/realizable turbulence model. Wind tunnel investigation was also carried out for the best-performed Savonius rotor configuration under the various parameters. Both simulation and experimental results were then compared for verification. In general, the results obtained showed that the performance of the Savonius rotor could be significantly improved by the addition of inner blades. The maximum enhancement of Cp was 41% for the case of single inner blade installed at 120o angle and tested at high TSR. As for the double inner blades, a maximum Cp of 13% was achieved when tested at low TSR (installed at 160o angle). The results also indicated that better performance of the Savonius rotor could be obtained when the spacing of inner blade was set at 0.02 m and 0.005 m for single and double inner blades, respectively. However, middle position of inner blades marked better performance for most of the cases. It can conclude that a significant enhancement of Savonius rotor performance can be achieved without high production cost and complex design involved. This solution would be very useful for generating high electricity in rural areas with a low cost 2020-09 Thesis http://eprints.uthm.edu.my/912/ http://eprints.uthm.edu.my/912/1/24p%20MOHANAD%20AL-GHRIYBAH.pdf text en public http://eprints.uthm.edu.my/912/3/MOHANAD%20AL-GHRIYBAH%20COPYRIGHT%20DECLARATION.pdf text en staffonly http://eprints.uthm.edu.my/912/2/MOHANAD%20AL-GHRIYBAH%20WATERMARK.pdf text en validuser phd doctoral Universiti Tun Hussein Onn Malaysia Fakulti Kejuruteraan Mekanikal dan Pembuatan |
| institution |
Universiti Tun Hussein Onn Malaysia |
| collection |
UTHM Institutional Repository |
| language |
English English English |
| topic |
TL500-777 Aeronautics Aeronautical engineering |
| spellingShingle |
TL500-777 Aeronautics Aeronautical engineering Al-Ghriybah, Mohanad Aerodynamic performance evaluation of multi inner blades savonius rotor |
| description |
Savonius wind turbine is the cheapest and simplest type of vertical axis wind
turbines. This turbine is being utilized in various countries due to the simplistic
design and low construction cost. However, this turbine suffers from low efficiency.
For that, this study aims to increase the performance of the Savonius wind rotor in
order to generate more useful power. In the present study, the aerodynamics
performance of the Savonius wind turbine rotor with inner blades was investigated.
The effect of number of inner blades, angle of inner blades, position of inner blades,
and distance between the inner blades were evaluated under low and normal ranges
of Tip Speed Ratio (TSR) through simulation and experimental work. A numerical
investigation was adopted using ANSYS Fluent 19.1 software in order to determine
the aerodynamic performance such as power coefficient (Cp) and torque coefficient
(Ct). The numerical investigation was performed using two and three-dimensional
simulations based on k-Ɛ/realizable turbulence model. Wind tunnel investigation
was also carried out for the best-performed Savonius rotor configuration under the
various parameters. Both simulation and experimental results were then compared
for verification. In general, the results obtained showed that the performance of the
Savonius rotor could be significantly improved by the addition of inner blades. The
maximum enhancement of Cp was 41% for the case of single inner blade installed at
120o
angle and tested at high TSR. As for the double inner blades, a maximum Cp of
13% was achieved when tested at low TSR (installed at 160o
angle). The results also
indicated that better performance of the Savonius rotor could be obtained when the
spacing of inner blade was set at 0.02 m and 0.005 m for single and double inner
blades, respectively. However, middle position of inner blades marked better
performance for most of the cases. It can conclude that a significant enhancement of
Savonius rotor performance can be achieved without high production cost and
complex design involved. This solution would be very useful for generating high
electricity in rural areas with a low cost |
| format |
Thesis |
| qualification_name |
Doctor of Philosophy (PhD.) |
| qualification_level |
Doctorate |
| author |
Al-Ghriybah, Mohanad |
| author_facet |
Al-Ghriybah, Mohanad |
| author_sort |
Al-Ghriybah, Mohanad |
| title |
Aerodynamic performance evaluation of multi inner blades savonius rotor |
| title_short |
Aerodynamic performance evaluation of multi inner blades savonius rotor |
| title_full |
Aerodynamic performance evaluation of multi inner blades savonius rotor |
| title_fullStr |
Aerodynamic performance evaluation of multi inner blades savonius rotor |
| title_full_unstemmed |
Aerodynamic performance evaluation of multi inner blades savonius rotor |
| title_sort |
aerodynamic performance evaluation of multi inner blades savonius rotor |
| granting_institution |
Universiti Tun Hussein Onn Malaysia |
| granting_department |
Fakulti Kejuruteraan Mekanikal dan Pembuatan |
| publishDate |
2020 |
| url |
http://eprints.uthm.edu.my/912/1/24p%20MOHANAD%20AL-GHRIYBAH.pdf http://eprints.uthm.edu.my/912/3/MOHANAD%20AL-GHRIYBAH%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/912/2/MOHANAD%20AL-GHRIYBAH%20WATERMARK.pdf |
| _version_ |
1747830712100192256 |