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JOURNAL OF ENGINEERING THERMOPHYSICS Apr., 2013
2013
1,2 1,3 1,2 1,3
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(1.
100190
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Joukowsky
NREL Phase VI
:TK83 :A : 0253–231X(2013)04–0646–04
The Viscous and Inviscid Interaction Aerodynamic
Model for HAWT
WANG Qiang1,2 XU Yu1,3 WANG Sheng-Jun1,2 XU Jian-Zhong1,3
(1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100190, China;
2. Graduate School of Chinese Academy of Sciences, Beijing 100049, China;
3. Key Laboratory of Wind Energy Utilization, Chinese Academy of Sciences, Beijing 100190, China)
Abstract The 3D Panel Method can obtain the 3D potential flow field just by the surface mesh
attached to the wind turbine blade and give accurate pressure coefficient distribution et. 3D flow
information without consuming too putational time. So the 3D Panel Method provides an
efficient access to the analysis of 3D flow field of HAWT. The boundary layer model is an efficient
method for analyz
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