| 摘要: |
| 在常温、超声速流动状态下,采用PIV技术定量测量了收敛喷管和收扩喷管加装小突片时射流纵截面的速度场和涡量场,并对其速度场和涡量场进行了比较。结果表明,对于收扩喷管,虽然其速度边界层厚度明显大于收敛喷管,但加装小突片结构也能够明显的强化射流的混合。并且发现,小突片结构不仅能产生流向涡,而且对周向涡有明显的强化作用。 |
| 关键词: 小突片+ 射流喷管 喷射流混合流 涡流 |
| DOI： |
| 分类号:V231.3 |
| 基金项目:国防科技预研基金资助 (0 0J1 0 5 2HK0 1 ) |
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| PIV measurements of the jet flows enhanced by tabs fixed on convergent-divergent (C-D) nozzles |
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ZUO Xiu-juan,HUANG Yong,LI Yong,Yuan Hui-jing
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1.Coll. of Energy and Power Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;2.Dept. of Thermal Engineering, Tsinghua Univ., Beijing 100084, China;3.Dept. of Mechanics, Peking Univ., Beijing 100084, China
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| Abstract: |
| To study the jet mixing enhancement by small tabs, a PIV system was used to conduct two-dimensional measurements of supersonic air jet flows exhausted from a convergent nozzle and two convergent-divergent (C-D) nozzles. The instantaneous quantitative velocity and vorticity fields were obtained to analyze the characteristics of the mixing process in the jet flow. It was found that the tabs fixed on C-D nozzles also enhanced the jet mixing distinctly, although the boundary layers of the jets from C-D nozzles were greater than that from the convergent nozzle. And the tabs intensified the circumferential vortices greatly in addition to the generation of streamwise vortices. |
| Key words: Small tabs~+ Jet nozzle Jet mixing flow Vortex flow |
