期刊文献+
共找到4篇文章
< 1 >
每页显示 20 50 100
水平轴风力机专用翼型性能评估方法 被引量:1
1
作者 李星星 杨科 +1 位作者 张磊 刘强 《工程热物理学报》 EI CAS CSCD 北大核心 2013年第5期849-852,共4页
本文提出了风力机翼型完整的性能参数体系和相应的评估方法,并以此评估了CAS-W1翼型与DU翼型的性能特征。对翼型性能的评估侧重于失速特性、非设计点特性和翼型气动性能的稳定性。评估结果表明,相对于DU翼型,CAS-W1翼型系列设计点性能... 本文提出了风力机翼型完整的性能参数体系和相应的评估方法,并以此评估了CAS-W1翼型与DU翼型的性能特征。对翼型性能的评估侧重于失速特性、非设计点特性和翼型气动性能的稳定性。评估结果表明,相对于DU翼型,CAS-W1翼型系列设计点性能和非设计点性能较好,但是失速特性和性能稳定性需要优化。 展开更多
关键词 风力机专用翼型 气动性能评价 失速特性 稳定性参数
原文传递
Evaluation of the Thermodynamic Performance of the Traditional Passive Systems
2
作者 Antonio De Vecchi Simona Colajanni +2 位作者 Annalisa Lanza Volpe Miriam Noto Annalisa Palermo 《Journal of Energy and Power Engineering》 2013年第5期850-857,共8页
The energy consumption of buildings in urban areas is one of the greatest source of energy wasting and, consequently, ofincreasing of CO2 emission. Research is currently focused on the reduction of this consumption th... The energy consumption of buildings in urban areas is one of the greatest source of energy wasting and, consequently, ofincreasing of CO2 emission. Research is currently focused on the reduction of this consumption through the use of passive air-conditioning systems, that can be integrated with conventional systems and give rise to the so-called hybrid systems. Historically, these passive systems were developed in the Mediterranean and Middle East area. The research approach on this topic involves the application of design strategies and the development of computational tools and control systems. The development of the hybrid systems is the result of the synergy between current scientific knowledge, advanced manufacturing and information technology. In this study, a modular housing system has been investigated under different conditions. Simulations have been repeated, in order to identify the configuration that provides the highest indoor comfort. The analysis of the different conditions has been carried out using a CFD (computational fluid dynamic) software. The paper shows the results developed by the Dipartimento di Architettura of the Universit^t di Palermo in the analysis of the natural ventilation effect on the indoor comfort. 展开更多
关键词 BUILDING CFD simulation passive systems energy saving.
下载PDF
超紧凑涡轮过渡段流动特征与优化设计研究 被引量:3
3
作者 梅艳梅 张伟昊 +1 位作者 刘火星 邹正平 《工程热物理学报》 EI CAS CSCD 北大核心 2019年第9期2012-2020,共9页
对某型带支板超紧凑涡轮级间过渡段进行了数值模拟,讨论了综合评价过渡段气动性能的方法,分析了超紧凑过渡段内典型流动特征,并针对该超紧凑过渡段进行了改型设计。结果表明,考虑压缩性、面积比、出口面选取等影响因素的扩压效率计算能... 对某型带支板超紧凑涡轮级间过渡段进行了数值模拟,讨论了综合评价过渡段气动性能的方法,分析了超紧凑过渡段内典型流动特征,并针对该超紧凑过渡段进行了改型设计。结果表明,考虑压缩性、面积比、出口面选取等影响因素的扩压效率计算能更加合理的描述过渡段扩压性能;超紧凑过渡段中机匣流动分离以及支板表面径向流动较强,从而形成复杂的二次流动结构,导致超紧凑过渡段内流动损失增加,是超紧凑过渡段内典型的流动特征;通过优化机匣和轮毂局部曲率,同时合理调整支板厚度分布和流向面积分布,优化设计后的超紧凑过渡段叶栅效率提高了4%,扩压效率提高了10.8%,出口面二次流动能减小了38%。 展开更多
关键词 超紧凑过渡段 气动性能评价 流动结构 二次流动能 优化设计
原文传递
A study on performance influences of airfoil aerodynamic parameters and evaluation indicators for the roughness sensitivity on wind turbine blade 被引量:14
4
作者 HUANG ChenWu YANG Ke +3 位作者 LIU Qiang ZHANG Lei BAI JingYan XU JianZhong 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第11期2993-2998,共6页
The roughness increase on horizontal axis wind turbine(HAWT) blade surface,especially on the leading edge,can lead to an aerodynamic performance degradation of blade and power output loss of HAWT,so roughness sensitiv... The roughness increase on horizontal axis wind turbine(HAWT) blade surface,especially on the leading edge,can lead to an aerodynamic performance degradation of blade and power output loss of HAWT,so roughness sensitivity is an important factor for the HAWT blade design.However,there is no criterion for evaluating roughness sensitivity of blade currently.In this paper,the performance influences of airfoil aerodynamic parameters were analyzed by the blade element momentum(BEM) method and 1.5 MW wind turbine blade.It showed that airfoil lift coefficient was the key parameter to the power output and axial thrust of HAWT.Moreover,the evaluation indicators of roughness sensitivity for the different spanwise airfoils of the pitch-regulated HAWT blade were proposed.Those respectively were the lift-to-drag ratio and lift coefficient without feedback system,the maximum lift-to-drag ratio and design lift coefficient with feedback system for the airfoils at outboard section of blade,and lift coefficient without feedback,maximum lift coefficient with feedback for the airfoils at other sections under the pitch-fixed and variable-speed operation.It is not necessary to consider the roughness when HWAT can be regulated to the rated power output by the pitch-regulated and invariable-speed operation. 展开更多
关键词 HAWT BLADE AIRFOIL aerodynamic performance roughness sensitivity evaluation indicator
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部