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首页> 外文期刊>Journal of Mechanical Science and Technology >Effects of a blade profile, the Reynolds number, and the solidity on the performance of a straight bladed vertical axis wind turbine
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Effects of a blade profile, the Reynolds number, and the solidity on the performance of a straight bladed vertical axis wind turbine

机译:叶片轮廓,雷诺数和坚固性对直叶片垂直轴风力发电机性能的影响

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This study investigates the effects of parameters such as a blade profile (changing the digit of the 4-digit NACA00xx airfoil), the Reynolds number, and the solidity on the performance characteristics of a straight bladed vertical axis wind turbine (VAWT). A numerical analysis, adopting the multiple stream tube (MST) method, is carried out to evaluate the performance depending on the parameters. The numerical result shows that the variation of a blade profile directly influences the power production, i.e., the high-digit NACA00xx airfoil provides higher power in a low speed zone (BSR < 3; BSR: blade speed ratio (ΩR/U_f), Ω: angular velocity of blade, R: radius of a straight Darrieus wind turbine, U_f: free stream velocity) than the low-digit NACA00xx profile. On the contrary, the low-digit NACA00xx airfoil produces higher power in a high speed range (BSR > 5) than the high-digit NACA00xx profile. An enhancement of the power production is observed with increasing the Reynolds number on the whole tested blade speed ratio range (1 < BSR < 12). In particular, the rate of the enhancement of the power is rapidly decreased with the increases of the Reynolds number (Re =ρU_rc/μ, ρ: air density, U_r: mean resultant velocity acting on a blade with variable rotating speeds in a uniform free stream velocity (U_f), c: blade chord length, μ: air viscosity). For the effect of the solidity on the power production, a marked reduction of the range of the blade speed ratio that can provide the power is observed with increasing the solidity. A pattern of very steep variation of the power around the peak in the low speed zone (BSR < 3) is found in a high solidity range (σ > 0.3; σ: solidity (Nc/R), N: number of blade, c: chord length of an airfoil), and this tendency is conspicuously different from that of the eggbeater-type Darrieus VAWT, which is interpreted as a gradual variation of the power around the peak.
机译:这项研究调查了诸如叶片轮廓(更改4位数的NACA00xx机翼的位数),雷诺数和坚固性等参数对直叶片垂直轴风力涡轮机(VAWT)的性能特性的影响。进行了采用多流管(MST)方法的数值分析,以根据参数评估性能。数值结果表明,叶片轮廓的变化直接影响功率产生,即高位NACA00xx机翼在低速区域(BSR <3; BSR:叶片速度比(ΩR/ U_f),Ω)提供更高的功率:叶片的角速度,R:直达里厄斯风力涡轮机的半径,U_f:自由流速度),其数值低于低位数的NACA00xx曲线。相反,低位NACA00xx机翼在高速范围(BSR> 5)中产生的功率大于高位NACA00xx轮廓。在整个测试叶片速度比范围(1 0.3;σ:固结度(Nc / R),N:叶片数,c)中,发现低速区域(BSR <3)周围的功率非常陡峭的变化模式。 :翼型的弦长),并且这种趋势与打蛋器型Darrieus VAWT的显着不同,后者被解释为峰值附近功率的逐渐变化。

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