...
首页> 外文期刊>Journal of Cleaner Production >Optimization of airfoil Based Savonius wind turbine using coupled discrete vortex method and salp swarm algorithm
【24h】

Optimization of airfoil Based Savonius wind turbine using coupled discrete vortex method and salp swarm algorithm

机译:基于翼型的芳瓦利乌斯风力涡轮机的优化使用耦合离散涡流法和SALP群算法

获取原文
获取原文并翻译 | 示例

摘要

In this research study, the optimization study of an airfoil type Savonius turbine is presented, focusing on maximizing the power coefficient. For this purpose, a Discrete Vortex Method (DVM) code for calculating power coefficient, a Class Shape Transfer (CST) function code for generating coordinates of airfoils and a Salp Swarm Algorithm (SSA) code for optimization have been developed. These three codes are coupled and an optimization procedure is generated. The decision variables of the mentioned problem are the CST function coefficients and the objective is the power coefficient. For verification of the results, CFD simulations are utilized. The results indicate that the achieved geometry could increase the power coefficient of a conventional Savonius turbine up to 27%. Also, the physical results indicate that the suction area and pressure magnitude of the pressure side of the airfoil type turbine is more extensive than simple type Savonius turbine at the optimization TSR. Therefore, in the airfoil type wind turbine, the great pressure difference causes more force at the surface of blades and in results, an increase in power coefficient occurs. (C) 2019 Elsevier Ltd. All rights reserved.
机译:在本研究研究中,提出了翼型式Savonius涡轮机的优化研究,专注于最大化功率系数。为此目的,已经开发了一种用于计算功率系数的离散涡流方法(DVM)代码,用于产生用于产生坐标的坐标和SALP群算法(SSA)代码进行优化的坐标。这三个代码耦合,并生成优化过程。所提到的问题的决策变量是CST功能系数,目标是功率系数。为了验证结果,使用CFD仿真。结果表明,实现的几何形状可以将传统的Savonius涡轮机的功率系数提高至27%。而且,物理结果表明,翼型涡轮机的压力侧的抽吸区域和压力幅度比优化TSR的简单型Savonius涡轮更广泛。因此,在翼型式风力涡轮机中,大的压力差导致叶片表面的力和结果,发生的功率系数的增加。 (c)2019 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号