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Secondary flow in ultra-low-aspect-ratio transonic turbine cascades.

超低展弦比跨音速涡轮叶栅中的二次流。

基本信息

批准号：
258090413
负责人：
Professor Dr.-Ing. Konrad Vogeler
金额：
--
依托单位：
Professur für Turbomaschinen und Flugantriebe
依托单位国家：
德国
项目类别：
Research Grants
财政年份：
2014
资助国家：
德国
起止时间：
2013-12-31 至 2017-12-31
项目状态：
已结题

来源：
https://gepris.dfg.de/gepris/projekt/258090413?language=en
关键词：
Secondary flow ultra low aspect

项目摘要

The proposed project will deliver a deeper understanding for the secondary loss effects in transonic turbine cascades with very low aspect ratio. As a result the existing loss correlation will be refined and extended for this extreme geometry range. Current public loss correlations do not cover the extreme low aspect ratio range. The planned investigations will imply the subsonic and transonic flow regime as well, since the transonic flow is very usual for the real applications.A typical phenomenon in configurations with a low endwall distance is the merging of the secondary flow effects. This effect, its influence on the main flow and the resulting flow losses are not yet investigated adequately.To create the database for the loss correlation extension, it is planned to use a hybrid approach, in which the data will be delivered by validated numerical investigations. For the validation special geometries will be investigated in a transonic cascade test rig. Using numerical data for the loss database enhances the flexibility and range of the investigation. Own previous work on this topic showed that the CFD is capable to predict the losses in this geometry. Moreover the cascade flow will be investigated in off-design conditions. This is important since the public incidence loss correlations are also not valid for the very low aspect ratio range. These flow regimes are also not understood. The project is not only important from a scientific point of view. The validated loss correlations in the very low aspect ratio range will be used in the design of high pressure air turbines. These turbines are for example used as engine simulators for wind tunnel tests of airplane models. Other applications are compressed air motors with very high rotation speed in the medicine industry and all other industries where compressed air motors with their very high power density are preferred over electrical motors.

该项目的提出将提供一个更深入的了解二次损失的影响，跨音速涡轮机叶栅与非常低的展弦比。因此，现有的损失相关性将被细化并扩展到这个极端的几何范围。目前的公共损失相关性不包括极低的长宽比范围。由于跨音速流动在真实的应用中是非常常见的，因此计划的研究也将包括亚音速和跨音速流动。在端壁距离较短的构型中，一个典型的现象是二次流效应的合并。这种效应及其对主流的影响和由此产生的流动损失尚未得到充分研究。为了创建损失相关扩展的数据库，计划使用混合方法，其中数据将通过验证的数值研究提供。为了验证，将在跨音速叶栅试验台上研究特殊的几何形状。损失数据库采用数字数据，可提高调查的灵活性和范围。自己以前在这方面的工作表明，CFD能够预测这种几何形状的损失。此外，叶栅流动将在非设计条件下进行研究。这一点很重要，因为公共入射损失相关性对于非常低的展弦比范围也是无效的。这些流态也不被理解。这个项目不仅从科学的角度来看很重要。在非常低的展弦比范围内验证的损失相关性将用于高压空气涡轮的设计。这些涡轮机例如用作飞机模型风洞试验的发动机模拟器。其他应用是在医药行业和所有其他行业中具有非常高转速的压缩空气马达，其中具有非常高功率密度的压缩空气马达优于电动马达。