首页> 外文OA文献 >Computing combustion noise by combining Large Eddy Simulation with analytical models for the propagation of waves through turbine blades
【2h】

Computing combustion noise by combining Large Eddy Simulation with analytical models for the propagation of waves through turbine blades

机译:通过将大涡模拟与解析模型结合使用来计算燃烧噪声,以通过涡轮叶片传播波

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

Two mechanisms control combustion noise generation as shown by Marble and Candel [1]: direct noise, in which acoustic waves propagate through the turbine stages and indirect noise, in which vorticity and/or entropy waves generate noise as they are convected through turbine stages. A method to calculate combustion-generated noise has been implemented in a tool called CHORUS. The method uses the Large eddy simulations of the combustion chamber obtained with the unstructured solver AVBP developed at CERFACS [2] and analytical models for the propagation through turbine stages. The propagation models [3] use the compact row hypothesis to write matching conditions between the inlet and the outlet of a turbine stage. Using numerical simulations, the validity of the analytical methods is studied and the errors made quantified.
机译:如Marble和Candel [1]所示,有两种机制可控制燃烧噪声的产生:直接噪声和间接噪声,其中直接声波通过涡轮机级传播,而间接噪声则是涡流和/或熵波在通过涡轮机级对流时产生噪声。一种计算燃烧产生的噪声的方法已经在称为CHORUS的工具中实现。该方法使用由CERFACS [2]开发的非结构化求解器AVBP获得的燃烧室的大涡模拟和用于透平级传播的分析模型。传播模型[3]使用紧凑行假设来写出涡轮级进口和出口之间的匹配条件。使用数值模拟,研究了分析方法的有效性并量化了误差。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号