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SECOND VANE TOTAL PRESSURE LOSS DUE TO ENDWALL ICEFORM CONTOURING

机译:端壁冰封轮廓造成的第二叶片总压力损失

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The iceformation design method generates an endwall contour, altering the secondary flows that produce elevated endwall heat transfer load and total pressure losses. Iceformation is an analog to regions of metal melting where a hot fluid alters the isothermal surface shape of a part as it is maintained by a cooling fluid. The passage flow, heat transfer and geometry evolve together under the constraints of flow and thermal boundary conditions. The iceformation concept is not media dependent and can be used in analogous flows and materials to evolve novel boundary shapes. In the past, this method has been shown to reduce aerodynamic drag and total pressure loss in flows such as diffusers and cylinder/endwall junctures. A prior paper [1] showed that the Reynolds number matched iceform geometry had a 24% lower average endwall heat transfer than the rotationally symmetric endwall geometry of the Energy Efficiency Engine (E3). Comparisons were made between three endwall geometries: the 'iceform', the 'E3' and the 'flat' as a limiting case of the endwall design space.This paper adds to the iceformation design record by reporting the endwall aerodynamic performances. Second vane exit flow velocities and pressures were measured using an automated 2-D traverse of a 1.2 mm diameter five-hole probe. Exit plane maps for the three endwall geometries are presented showing the details of the total pressure coefficient contours and the velocity vectors. The formation of secondary flow vortices is shown in the exit plane and this results in an impact on exit plane total pressure loss distribution, off-design over-and under-turning of the exit flow. The exit plane contours are integrated to form overall measures of the total pressure loss. Relative to the E3 endwall, the iceform endwall has a slightly higher total pressure loss attributed to higher dissipation of the secondary flow within the passage. The iceform endwall has a closer-to-design exit flow pattern than the E3 endwall.
机译:冰形成设计方法生成端壁轮廓,从而改变二次流,从而产生升高的端壁传热负荷和总压力损失。冰的形成类似于金属熔化的区域,在该区域中,热流体会改变零件的等温表面形状,而该等温表面形状是由冷却流体保持的。在流动和热边界条件的约束下,通道的流动,传热和几何形状一起发展。冰层形成的概念不依赖于介质,可以用于类似的流动和材料中,以演化出新颖的边界形状。过去,这种方法已被证明可以减少空气动力阻力和流(例如扩散器和气缸/端壁接合处)中的总压力损失。先前的论文[1]显示,与能源效率引擎(E3)的旋转对称端壁几何形状相比,与雷诺数匹配的冰形几何形状的平均端壁传热降低了24%。比较了三种端壁几何形状:“ iceform”,“ E3”和“ flat”作为端壁设计空间的极限情况。 本文通过报告端壁的空气动力学性能,将其添加到冰形成设计记录中。使用直径为1.2 mm的五孔探头的自动2-D导线测量第二叶片出口的流速和压力。给出了三种端壁几何形状的出口平面图,显示了总压力系数轮廓和速度矢量的详细信息。在出口平面上显示了二次流动涡流的形成,这会影响出口平面的总压力损失分布,出口流量的非设计上翻和下翻。出口平面轮廓被整合以形成总压力损失的整体度量。相对于E3端壁,冰状端壁的总压力损失略高,这归因于通道内二次流的较高耗散。与E3端壁相比,冰形端壁的出口流型更接近设计。

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