共查询到19条相似文献,搜索用时 93 毫秒
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旋转离心叶轮与叶片扩压器间耦合流动的数值分析 总被引:3,自引:1,他引:2
以离心压气机内部动静部件耦合的非定常流场为研究对象,本文提出了动静耦合统一正命题型式,采用κ-ε紊流模型、同步计算动静耦合流场的方法,分别对下同流量工况下离心叶轮与叶片扩压器内部非定常流动进行了数值计算。计算结果与激光多普勒测量结果进行了比较:在设计工况下,离心叶轮与叶片扩压器相互匹配较好,而在非设计工况下,流道内流动趋向恶化。说明计算结果是有一定的可信度;计算结果同时说明,只有采用非定常算法,才有可能较好地描述动静部件耦合的流场。 相似文献
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众所周知,叶轮出口流场的特性反映了叶轮内部流动状况,对研究叶轮内部流动机理十分重要。轴流叶轮内的流动,由于粘性的影响,气体在环壁区域呈现为顶端间隙泄漏、环壁边界层、二次流以及壁面失速等复杂的流动现象。对于不同场合用的轴流机械,即使在设计工况下,这些流动现象的表现和干涉程度也不相同,因此适用于任意设计条件下环 相似文献
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对向心透平叶轮内部复杂流动在级环境下进行了全三维黏性数值模拟,结合拓扑学原理分析了设计工况和非设计工况下其内流动分离及各种涡系发展的演变过程,初步建立了向心透平叶轮内的旋涡模型,阐述了流动损失的形成机理。研究表明:向心透平叶轮内部涡系与轴流式透平存在较大差别,且流动分离及涡系主要集中在吸力面侧;设计工况下向心透平叶轮内的主要旋涡包括马蹄涡、通道涡及泄漏涡,其主要表现为通道涡与泄漏涡相互影响和掺混,是主要损失的形成原因;非设计工况下,主流在叶轮叶片前缘处发生大范围的分离及回流,造成了较大的能量损失,但二次流损失所占比例较小。 相似文献
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离心式流体机械内,特别是离心叶轮内部的流动相当复杂,单靠理论计算来正确预测叶轮内部流态和设计高效率的叶轮是有困难的。七十年代以来,运用三元流动理论和流动分析法求解叶轮内流场分布获得很大进展,但由于粘性对叶轮壁面的影响和叶轮出、入口的边界条件不易确定,计算结果与真实流动模型尚有一定差距。因此用实验方法 相似文献
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为了探讨叶型弯曲不同分布对叶轮效率的影响,本文使用三元粘性数值模拟方法,对几个具有弯曲母线的离心叶轮进行了分析比较,在减损机理、特别是设计准则方面进行了摸索和探讨。 相似文献
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切线泵整机多相位定常流动数值模拟 总被引:6,自引:2,他引:4
本文对一单级切线泵在设计工况进行了多相位定常流动数值模拟,分析了由于叶轮与蜗壳相对位置的变化引起的泵的扬程、叶轮流道内的质量流量、速度场、压力场的变化规律。计算表明,切线泵内流场非常复杂,整机多相位定常流动数值模拟的结果实际上是泵内流场非定常特性在定常计算中的反映,其内部流动呈周期性变化,叶轮流道在不同的位置流动情况差别很大。本次计算为进一步提高切线泵性能、减少水力损失提供了一定的理论依据。 相似文献
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关于Krain实验叶轮几何型线及其流道二次流旋涡结构的讨论 总被引:10,自引:1,他引:9
Krain关于高速离心式压缩机叶轮内部流畅的LDA实验测量不仅对认识这种特定的复杂流动有重要意义,而且亦为验证正在迅速发展的CFD软件提供了比较依据。但是作者发现,Krain公开发表的实验叶轮的几何型线缺少叶轮出口附近区域的型线坐标,直接用其进行数值计算分析将引起误差。为此,本文根据Krain在不同文献中所提供的有关实验叶轮的资料,重新构造补全了实验叶轮出口区域的型线坐标。然后,利用一多功能CFD软件对该实验叶轮进行了计算分析,较详细、深入地探讨了叶轮流道内二次流旋涡结构的形成和发展过程。 相似文献
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Laser velocimetries, such as LDV or laser-2-focus (L2F) velocimetry, have been widely used for a flow measurement in a high-speed rotating impeller. A particle image velocimetry (PIV) is one of the popular velocity measurement techniques for the ability to measure a velocity field. And a PIV offers an extensive velocity field in an extremely shorter measurement time than the laser velocimetries. In the present experiment, a PIV was applied to a flow measurement in a transonic centrifugal impeller. A phase locked measurement technique every 20% blade pitch was performed to obtain a velocity field over one blade pitch of the inducer. The measured velocity field at the inducer of impeller clearly showed a shock wave generated on the suction surface of a blade. The validity of the present technique was also discussed. 相似文献
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A numerical study on the flow and sound fields of centrifugal impeller located near a wedge 总被引:3,自引:0,他引:3
Centrifugal fans are widely used and the noise generated by these machines causes one of the serious problems. In general, the centrifugal fan noise is often dominated by tones at blade passage frequency and its higher harmonics. This is a consequence of the strong interaction between the flow discharged from the impeller and the cut-off in the casing. However, only a few researches have been carried out on predicting the noise because of the difficulty in obtaining detailed information about the flow field and considering the scattering effect of the casing. The objective of this study is to understand the generation mechanism of sound and to develop a prediction method for the unsteady flow field and the acoustic pressure field of the centrifugal impeller. A discrete vortex method is used to model the centrifugal impeller and a wedge and to calculate the flow field. The force of each element on the blade is calculated by the unsteady Bernoulli equation. Lowson's method is used to predict the acoustic source. In order to consider the scattering and diffraction effects of the casing, Kirchhoff-Helmholtz boundary element method (BEM) is developed. The source of Kirchhoff-Helmholtz BEM is newly developed, so the sound field of the centrifugal fan can be obtained. A centrifugal impeller and wedge are used in the numerical calculation and the results are compared with the experimental data. Reasonable results are obtained not only for the peak frequencies but also for the amplitudes of the tonal sound. The radiated acoustic field shows the diffraction and scattering effect of the wedge. 相似文献