• 主题
高级搜索  >
历史搜索 清空历史
首页> 外文会议>International Symposium on Air Breathing Engines >INVESTIGATION OF THE INFLUENCE OF STREAMWISE VORTICES GENERATING GEOMETRIES OF STRUT INJECTORS ON THE MIXING AND COMBUSTION PROCESS IN A SCRAMJET MODEL COMBUSTOR
【24h】

INVESTIGATION OF THE INFLUENCE OF STREAMWISE VORTICES GENERATING GEOMETRIES OF STRUT INJECTORS ON THE MIXING AND COMBUSTION PROCESS IN A SCRAMJET MODEL COMBUSTOR

机译：Scrut喷射器生成几何对汽轮模型燃烧室混合和燃烧过程的影响的研究

获取原文
页面导航
  • 摘要
  • 著录项
  • 相似文献
  • 相关主题

摘要

The influence of two different outer contours of wedge shaped hydrogen injectors on the flow field and the mixing and combustion characteristics in a scramjet model combustion chamber was investigated. Various diagnostic techniques were applied in this detailed examination. It could be shown that the surface geometry of the inject-tors and the resulting potential to produce streamwise vortices for mixing enhancement has a distinct influence on the combustion process and the related heat release inside the combustor. The results of wall static pressure measurements under nonreacting test case conditions are similar for both injectors, which indicate similar flow fields. In the reacting test case, however, the wall pressure increase is signifycantly different, which indicates different rates of heat release within the length of the combustor. Furthermore, it could be revealed that the three dimensional structure of the hydrogen-air contact surface depends on the injector, resulting from the unlike induction of the streamwise vortices by the dissimilar surface contours of the injectors.
机译：研究了楔形氢气喷射器对流场的影响及扰型模型燃烧室中的楔形氢气喷射器的影响。在此详细检查中应用了各种诊断技术。可以示出，注射件的表面几何形状和产生用于混合增强的流动涡流的所得电位对燃烧过程具有不同的影响和燃烧器内的相关热释放。在非反应性测试壳体条件下的壁静压测量结果对于两个喷射器相似，这表明了类似的流场。然而，在反应测试壳体中，壁压增加是表示性不同的，这表明燃烧器长度内的热释放速率不同。此外，它可以被显示，该氢气 - 空气接触面的三维结构依赖于喷射器，从由所述喷射器的不同表面轮廓不同于感应的流向涡的产生。

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