Zobrazeno 1 - 9
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pro vyhledávání: '"Changping Liang"'
Autor:
Changping Liang, Huaxing Li
Publikováno v:
Royal Society Open Science, Vol 5, Iss 7 (2018)
This paper reports on the optimization of the NACA0015 aerofoil for improving the power performance of a vertical axis wind turbine (VAWT). The target range of the chord Re is 3 × 105–106, the tip speed ratio (TSR) is 2–6 and the solidity is 0.2
Externí odkaz:
https://doaj.org/article/3c0e9af3b0cd40da91b5ec56bc9639ae
Publikováno v:
International Journal of Hydrogen Energy. 47:8130-8144
Publikováno v:
Microscopy Research and Technique. 85:1791-1798
To compare the clinical application value of positron emission tomography-computed tomography (PET-CT) and magnetic resonance imaging (MRI) in the diagnosis of cervical cancer lymph node metastasis. We searched PubMed and other databases for the stud
Publikováno v:
European Journal of Nuclear Medicine and Molecular Imaging. 50:2228-2229
Autor:
Changping Liang
Publikováno v:
Journal of Physics: Conference Series. 1600:012032
The two-dimensional numerical simulation for NACA0015 airfoil and S325 airfoil were conducted with k-ω SST turbulence model. For the k-ω SST turbulence model could not predict the airfoil stall characteristics accurately, the non-equilibrium turbul
Autor:
Huaxing Li, Changping Liang
Publikováno v:
Royal Society Open Science
Royal Society Open Science, Vol 5, Iss 7 (2018)
Royal Society Open Science, Vol 5, Iss 7 (2018)
This paper reports on the optimization of the NACA0015 aerofoil for improving the power performance of a vertical axis wind turbine (VAWT). The target range of the chord Re is 3 × 10 5 –10 6 , the tip speed ratio (TSR) is 2–6 and the solidity is
Autor:
Huaxing Li, Changping Liang
Publikováno v:
Journal of the Brazilian Society of Mechanical Sciences and Engineering. 40
This paper investigates the effects of optimized airfoil on VAWT (vertical axis wind turbine) aerodynamic performance. The thickness and camber of the airfoil are selected as the constraints, the value of the maximum tangential force coefficient is c
Optimizing the NACA0015 airfoil which is widely applied in small-scale vertical axis wind turbine to make it has a better aerodynamic performance. In the optimization process, using CST parameterization method to perturb the airfoil geometry, the thi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::79957f371e05396d98b1e538e5717eea
https://doi.org/10.20944/preprints201608.0136.v1
https://doi.org/10.20944/preprints201608.0136.v1
Publikováno v:
IOP Conference Series: Earth and Environmental Science. 170:042061