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Cited 2 time in webofscience Cited 2 time in scopus
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Effect of blade chord length on startup performance of H-type tidal current turbine rotoropen access

Authors
Wang, Z.Kang, C.Zhang, Y.Kim, Hyoung-BumJin, F.
Issue Date
Mar-2023
Publisher
American Institute of Physics Inc.
Citation
AIP Advances, v.13, no.3
Indexed
SCIE
SCOPUS
Journal Title
AIP Advances
Volume
13
Number
3
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/30830
DOI
10.1063/5.0141151
ISSN
2158-3226
2158-3226
Abstract
This study aims to reveal the effect of the blade chord length on the startup performance of the lift rotor that converts the kinetic energy of tidal currents. The computational fluid dynamics technique was used to simulate unsteady flows around the rotor. The six degrees of freedom method was adopted to model the correlation between the rotational speed of the rotor and influential torques acting on the rotor. A comparative analysis of transient flows, rotational speed, and output torque was implemented at different initial azimuthal angles. The results show that as the rotor starts up at the minimum torque, the time required to attain the maximum rotational speed is longer than that associated with the maximum torque. As the maximum rotational speed is reached, low-pressure elements are produced in the area enclosed by the rotor blades, which is insensitive to the initial setting angle. A large area of low pressure is responsible for low output torque. During the startup process, the rotational speed experiences stages of sharp increase, fluctuating decrease, and moderate fluctuation, as is common at different blade chord lengths. As the chord length increases from 0.16 to 0.24 m, the startup process is extended by 0.63 s, and the average rotational speed in the stabilization stage decreases. © 2023 Author(s).
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Kim, Hyoung Bum
대학원 (기계항공우주공학부)
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