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Local heat transfer downstream of an asymmetric abrupt expansion and cavity in a circular tube

机译:圆管中非对称突变和腔下游的局部传热

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This study is concerned with measuring local heat transfer downstream of an asymmetric abrupt expansion and an asymmetric abrupt expansion followed by an asymmetric abrupt contraction (called "asymmetric cavity") in a circular tube at a uniform wall temperature. The effects of geometry and three-dimensionality of the flow caused by asymmetric expansion on heat transfer characteristics are also examined. The flow just upstream of the expansion is unheated and fully developed at the entrance to the heated asymmetric abrupt expansion region. Local heat transfer coefficients are measured using a specially designed isothermal heat flux sensor. Measurements for the asymmetric abrupt expansion are made at a small to large diameter ratio of d/D = 0.4 and 0.533 for Reynolds numbers of Re_D = 17,300 and 21,900, respectively. The eccentricities of the tube axis (e/D) are 0.25 and 0.17 for d/D = 0.4, and 0.195 and 0.065 for d/D = 0.533. For the asymmetric cavity, all tests are made at d/D = 0.4 and Re_D = 17,300 with various cavity lengths for e/D = 0 and 0.25, respectively. For both cases, the variations of local Nusselt number are observed along the wall of downstream circular tube at several angular positions around the tube circumference. In general, the local Nusselt numbers downstream of an asymmetric abrupt expansion are substantially higher than the fully developed values for the range of Reynolds numbers, diameter ratios and eccentricities investigated, due to high turbulence and mixing action in the recirculation region. And the maximum Nusselt numbers occur between 10 and 15 step heights from the expansion step. The Nusselt number distributions for the asymmetric cavity show a dramatic increase to the maximum values as the downstream region of the cavity is approached. This behavior is attributed to a periodic vortex shedding, subsequent impingement on the downstream corner region of the cavity and three-dimensionality effects which cause an increase in turbulence intensity.
机译:这项研究与在均匀壁温下在圆形管中测量不对称突然膨胀和不对称突然膨胀接着不对称突然收缩(称为“不对称腔”)下游的局部传热有关。还研究了非对称膨胀引起的几何形状和三维流动对传热特性的影响。刚好在膨胀上游的流动是不加热的,并且在加热的非对称突变区域的入口处完全流动。使用专门设计的等温热通量传感器测量局部传热系数。对于Re_D的雷诺数分别为17,300和21,900,以小/大直径比d / D = 0.4和0.533进行非对称突然膨胀的测量。 d / D = 0.4时,管轴的偏心率(e / D)为0.25和0.17,d / D = 0.533时为0.195和0.065。对于非对称腔体,所有测试均在d / D = 0.4和Re_D = 17,300下进行,其中各种腔体长度分别为e / D = 0和0.25。对于这两种情况,沿着下游圆管的壁在围绕管圆周的多个角度位置处观察到局部努塞尔数的变化。通常,由于再循环区域中的高湍流和混合作用,非对称突然膨胀下游的局部Nusselt数显着高于所研究的雷诺数,直径比和偏心率范围的完全展开值。从展开步骤开始,最大努塞尔数出现在10到15个步骤高度之间。随着接近空腔的下游区域,非对称空腔的Nusselt数分布显示出极大的增加。此行为归因于周期性的涡旋脱落,随后对腔体下游角部区域的撞击以及三维效应,这些效应导致湍流强度增加。

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