首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.6 pt.A; 20050606-09; Reno-Tahoe,NV(US) >An Experimental Investigation of Secondary Flows and Loss Development Downstream of a Highly Loaded Low Pressure Turbine Outlet Guide Vane Cascade
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An Experimental Investigation of Secondary Flows and Loss Development Downstream of a Highly Loaded Low Pressure Turbine Outlet Guide Vane Cascade

机译:高负荷低压汽轮机出口导流叶栅下游二次流动和损失发展的实验研究

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摘要

This paper presents a detailed experimental investigation of the evolution of secondary flow field characteristics and losses at several measurement planes downstream of a highly loaded low pressure turbine/outlet guide vane (LPT/OGV). The experiments were carried out in a linear cascade at Chalmers in Sweden. Several realistic upstream incidences and turbulence intensities have been investigated for one Reynolds number. Downstream characteristics have been measured with a 5-hole pneumatic probe. This allows for the determination of the mean vortical structures, their development and their interactions. The passage vortex and the blade shed vorticity are clearly visible at different downstream positions. Their intensity is shown to be strongly dependent on the inlet flow angle. The turbulence level seems to play a role on both the mixing within, and between the structures. The measurements also show that the losses along the blade span are dependent on the development of these structures.
机译:本文对高负荷低压涡轮机/出口导流叶片(LPT / OGV)下游几个测量平面上的次级流场特性和损耗的演化进行了详细的实验研究。实验是在瑞典Chalmers的线性级联中进行的。对于一个雷诺数,已经研究了几种实际的上游发生率和湍流强度。下游特性已使用5孔气动探头进行了测量。这样就可以确定平均涡旋结构,其发展及其相互作用。通道涡流和叶片脱落涡流在不同的下游位置清晰可见。显示出它们的强度很大程度上取决于入口流动角度。湍流水平似乎在结构内部以及结构之间的混合中都起作用。测量结果还表明,沿叶片跨度的损耗取决于这些结构的发展。

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