首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Influence of geometry on the efficiency of convergent-divergent nozzles applied to Tesla turbines
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Influence of geometry on the efficiency of convergent-divergent nozzles applied to Tesla turbines

机译:几何形状对应用于Tesla涡轮机的收敛-发散喷嘴效率的影响

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摘要

Convergent-divergent (CD) nozzles were designed and manufactured to improve the injection efficiency of the working fluid in Tesla turbines. Ten nozzles have been designed using two different techniques: a one-dimensional approach and a two-dimensional approach with the method of characteristics. All nozzles had rectangular geometry at throat, while 3 had divergent section planar and 2 divergent section circular, considering each mass flow rate (55 and 70 kg h(-1)). Nozzles were analyzed using air as the working fluid. A nozzle exit to throat area ratio (NAR) of 1.35 was used in all nozzles, while the nozzle pressure ratios (NPR) ranged between 2.15 and 3.25. At planar nozzles an (x/H)(exit) of 2.1 was more suitable for decreased of total pressure losses, while at circular nozzles the shock waves were canceled inside of divergent section. (C) 2015 Elsevier Inc. All rights reserved.
机译:设计并制造了收敛-扩张(CD)喷嘴,以提高Tesla涡轮中工作流体的喷射效率。已经使用两种不同的技术设计了十个喷嘴:一维方法和具有特征方法的二维方法。考虑到每种质量流量(55和70 kg h(-1)),所有喷嘴的喉咙都具有矩形几何形状,而3个喷嘴的发散截面为平面,两个喷嘴的发散截面为圆形。使用空气作为工作流体分析喷嘴。所有喷嘴均使用1.35的喷嘴出口与喉部面积之比(NAR),而喷嘴压力比(NPR)在2.15至3.25之间。在平面喷嘴处,(x / H)(出口)的2.1更适合于降低总压力损失,而在圆形喷嘴处,冲击波在发散截面内被抵消。 (C)2015 Elsevier Inc.保留所有权利。

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