首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >INFLUENCE OF TIP JET MASS FLOW AND BLOWING RATE ON THE PERFORMANCE OF AN AXIAL DIFFUSER AT DIFFERENT INLET TOTAL PRESSURE PROFILES
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INFLUENCE OF TIP JET MASS FLOW AND BLOWING RATE ON THE PERFORMANCE OF AN AXIAL DIFFUSER AT DIFFERENT INLET TOTAL PRESSURE PROFILES

机译:尖端射流质量和流量对不同入口总压力分布下轴扩散器性能的影响

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The present paper evaluates the impact of casing energized jet flow on the performance of an annular-conical exhaust diffuser. Two different inflow profiles, namely a uniform total pressure and a hub-strong total pressure inlet profile were studied. For both profiles, the flow is observed to separate at the casing. Experiments were performed at different tip jet mass flow rates and two different tip gap heights to understand their effect on the diffuser performance. Apart from wall pressure readings, probe measurements have been done at various locations within the diffuser to study the flow behaviour in more detail. The results show that at the diffuser inlet already small tip jet flows help to prevent casing separation and hence improve pressure recovery noticeably, especially in the front section of the diffuser. On the other hand, higher tip jet flows tend to weaken the core flow at the diffuser exit, thus generating an inhomogeneous outflow velocity profile. To enhance the interpretation of the experimental data, results from Computational Fluid Dynamics (CFD) simulations are used. Interestingly, the experimental results indicate that while the blowing ratio seems to be the major parameter for the improvement of pressure recovery for a hub-strong inlet profile, the pressure recovery for a uniform profile appears to be more sensitive to the tip jet mass flow rate. However, the numerical results do not show this trend.
机译:本文评估了外壳激励射流对环形圆锥形排气扩压器性能的影响。研究了两种不同的流入曲线,即均匀的总压力和集线器强的总压力入口曲线。对于这两个剖面,观察到流量在套管处分离。在不同的喷嘴喷射质量流量和两个不同的喷嘴间隙高度进行实验,以了解它们对扩散器性能的影响。除壁压力读数外,还对扩散器内的各个位置进行了探头测量,以更详细地研究流动特性。结果表明,在扩压器进口处,已经很小的喷嘴喷射流有助于防止机壳分离,从而显着提高压力恢复能力,尤其是在扩压器的前部。另一方面,较高的尖端射流倾向于削弱扩散器出口处的芯流,从而产生不均匀的流出速度曲线。为了增强对实验数据的解释,使用了计算流体动力学(CFD)模拟的结果。有趣的是,实验结果表明,虽然鼓风比似乎是改善轮毂强进气口曲线压力恢复的主要参数,但均匀曲线的压力恢复似乎对尖端射流质量流量更敏感。但是,数值结果没有显示出这种趋势。

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