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Unsteady flow structures of a counter-rotating swirl cup

  • Yang Lin*
  • , Yu Zhen Lin
  • , Gao En Liu
  • *此作品的通讯作者
  • National Key Laboratory of Science and Technology on Aero Engines Aero-Thermodynamics
  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Swirl can form Central Toroidal Recirculation Zones (CTRZ) in the center of flow region and can cause a negative axial pressure to be set up in the vicinity of the axis, reducing the length of flame, stabilizing combustion and enhancing the mix of fuel/air. Understanding the characteristics of swirling flow, especially the dynamics of Large Coherent Structures (LCS) associated with swirl, are very important for achieving suppression of combustion instability and obtaining low-NOx emissions. The present study investigated the flow field characteristics of a counter-rotating swirl cup in a real model combustor of rectangular geometry under isothermal condition, using PIV. Two-dimension PIV is adopted as the diagnostic technique to obtain the velocity vector field in the plane along to the axis of the test section. The experiment was aimed at understanding the swirl flow field characteristics down stream the swirl cup. Apart from obtaining the mean and turbulent velocity data, the structure and length scales of the CTRZ obtained from PIV measurement are also described.

源语言英语
主期刊名45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
出版状态已出版 - 2009
活动45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit - Denver, CO, 美国
期限: 2 8月 20095 8月 2009

出版系列

姓名45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

会议

会议45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
国家/地区美国
Denver, CO
时期2/08/095/08/09

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