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波瓣喷管引射-混合器涡结构的数值研究 被引量:14

Numerical investigation of vortical structures in the lobed mixer-ejector
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摘要 通过波瓣喷管引射-混合器的流场三维数值计算,得到了流向涡和正交涡产生、衰减的演变以及对混合效率的影响规律,进一步揭示了波瓣喷管有利于强化引射能力和混合效率的内在机理。结果表明:喷管出口流向涡的尺度基本与波瓣的高度相当,流向涡可以诱发主流和次流之间强烈的对流混合,在喷管下游一倍混合管直径的混合距离内强化混合作用显著,随着流向涡向下游发展,涡强衰减迅速;正交涡具有与波瓣尾缘一样的几何外形,在混合管下游,由于主流和次流之间的速度梯度下降,正交涡的强度显著降低,对强化混合的影响不大。 Three-dimension flow fields in the lobed mixer-ejector is numerically investigated, with main focus on vortical structures as well as vortical characteristics, to reveal further mechanism of the lobed mixer-ejector on enhanced mixing efficiency and pumping capacity. The results show that : ( 1 ) the scale of streamwise vortices at the trailing edge of lobed nozzle is about the lobe height, the important contribution of the streamwise vortices for enhanced mixing occurs in downstream distance away from nozzle exit about one mixing duct diameter and then the intensity of streamwise vortices decays obviously; (2) the normal vortices take on lobed shape near the trailing edge of lobed nozzle, the normal vortices intensity decreases rapidly downstream, and have a little effect on enhanced mixing efficiency. These results are verified with the physics nature.
作者 单勇 张靖周
出处 《空气动力学学报》 EI CSCD 北大核心 2005年第3期355-359,共5页 Acta Aerodynamica Sinica
关键词 波瓣喷管 混合器 数值计算 流向涡 正交涡 lobed nozzle mixer numerical computation stream-wise vortices normal vortices
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参考文献13

  • 1张靖周,李立国,高潮,何文斌.波瓣喷管红外抑制系统的实验研究[J].航空动力学报,1997,12(2):212-214. 被引量:59
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二级参考文献18

  • 1张靖周,李立国,吴国钏.波瓣混合结构三维流场数值计算[J].南京航空航天大学学报,1996,28(6):745-749. 被引量:3
  • 2张靖周,李立国,高潮,何文斌.波瓣喷管红外抑制系统的实验研究[J].航空动力学报,1997,12(2):212-214. 被引量:59
  • 3[1]Presz W M, Reynolds G, McCormick D C. Thrust Augment Using Mixer-ejector-diffuser Systems [R]. AIAA 94- 0020.
  • 4[2]Presz W M. Mixer/Ejector Noise Suppressors[R]. AIAA 91-2243.
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