To better study the flame flowfield and structure in lean and premixed swirling flames
a premixed swirling burner with strong confined combustor was designed
and the experimental instantaneous and simultaneous system of PIV (particle image velocimetry) and OH-PLIF (planar laser-induced fluorescence) was built. With this system
the measurement research was carried out in swirling flame under typical operating condition
meanwhile time-averaged and instantaneous simultaneous flame velocity flowfield and OH distribution structures in multiple sections were obtained. Results showed that multiple flame reaction zones existed in the bottom corners of combustor under condition of unsteady combustion at low equivalence ratio
accompanied by flash back in corner vortices. Due to shear effect of swirling flow
lots of wrinkles appeared along the edge of OH distribution structure
and many isolated OH blocks were observed. The root of swirling flame lied at inner side of shear layer of the jet flow. As equivalence ratio increased
the swirling flame velocity flowfied and OH distribution structures were similar to low equivalence ratio. But the combustion was more stable
and the flame height increased somehow. It was found that the typical two vortices were split into multiple vortices sometime. There were phenomena with vortex moving and breaking down.
Study on thermoacoustic characteristic of lean premixed swirling flames
PIV measurement of water tunnel for the flow field of a hovering coaxial-rotor
基于三维接触摩擦单元的套齿连接解析建模研究
与发动机匹配的旁路式双喉道气动矢量喷管数值模拟研究
组合式弹性金属密封泄漏特性实验研究与结构优化
Related Author
YANG Fu-jiang
GUO Zhi-hui
ZENG Yu-hui
YU Shi-mei
DENG Yan-min
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics