首页> 外文会议>ASME gas turbine India conference >MODELING OF PARTICLE WALL INTERACTION AND FILM TRANSPORT USING EULERIAN WALL FILM MODEL
【24h】

MODELING OF PARTICLE WALL INTERACTION AND FILM TRANSPORT USING EULERIAN WALL FILM MODEL

机译:使用EULERIAN壁膜模型对颗粒壁相互作用和膜传输进行建模

获取原文

摘要

The growing awareness of pollutant emissions from gas turbines has made it very important to study fuel atomization system, the spray wall interaction and hydrodynamic of film formed on engine walls. A precise fuel spray spatial distribution and efficient fuel air mixing plays important role in improving combustion performance. Cross-flow injection and film atomization technique has been studied extensively for gas turbine engines to achieve efficient combustion. Air blast atomizer is one of these kind of systems used in gas turbine engines which involves shear driven prefilmer secondary atomization. In addition to gas turbine combustor shear driven liquid wall film can be seen in IC engines, rocket nozzles, heat exchangers and also on steam turbine blades. In our work we have used Eulerian Wall Film (EWF) model to simulate the experiment performed by Arienti et al. In the Arienti's experiment liquid jet is injected from a nozzle from the top of the chamber. Droplets shed from the jet surface due to primary and later secondary atomization in the presence of high shearing cross flowing air. Further liquid fuel particles hit the wall to form film, film moves subjected to shear from the gas phase. Liquid film can reatomizes due to subgrid processes like stripping, splashing and film breakup. In current study we have validated Arienti et al. experimental data by modeling complex & coupled physics of spray, film and continuous phase and by accounting complex subgrid processes.
机译:燃气轮机污染物排放的越来越高的意识已经使研究燃料雾化系统,在发动机壁上形成的膜的喷射壁相互作用和流体动力学非常重要。精确的燃料喷雾空间分布和高效燃料空气混合在提高燃烧性能方面起着重要作用。已经广泛研究了横流注射和薄膜雾化技术,以实现燃气涡轮发动机以实现有效的燃烧。空气鼓雾雾化器是燃气涡轮发动机中使用的这些系统之一,其涉及剪切驱动的Previler二次雾化。除了燃气轮机燃烧器剪切驱动的液体壁膜,可以在IC发动机,火箭喷嘴,热交换器和蒸汽轮机叶片上看到。在我们的工作中,我们使用了eulerian墙膜(EWF)模型来模拟Arienti等人进行的实验。在Arienti的实验中,液体射流从腔室顶部从喷嘴注入。由于初级和后期的二次雾化在高剪切十字流动空气存在下,从喷射表面脱落。进一步的液体燃料颗粒撞击壁以形成薄膜,膜移动对气相剪切。由于剥离,飞溅和薄膜分解,液体膜可以引起的亚底工艺引起重化。在目前的研究中,我们已经验证了Arienti等。通过模拟喷涂,薄膜和连续相位的复杂和耦合物理学和通过算起复杂的底片过程来进行实验数据。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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