Investigation on Mixing Behavior of Seeping Gas Film in Supersonic Boundary Layer Based on Acetone Planar Laser-Induced Fluorescence

IF 0.6 4区 工程技术 Q4 MECHANICS
Q. Mi, S. K. Chen, S. H. Yi, D. D. Gang, F. Yuan
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Abstract

Porous media seepage flow is the active flow control method used to reduce heat and skin friction in high-speed vehicles, but effective measurement techniques for mixing the seeping gases with the incoming boundary layer are lacking. By premixing approximately 20% acetone vapor in the cooling gas and employing the acetone planar laser-induced fluorescence (PLIF) technology, flow of the seeping gas film within the boundary layer was visualized. A correlation between the relative intensity of PLIF image grayscale and the gas film mixing rate is established. Experimental results showed that the seeping gas film layer remains initially laminar in the Mach 3 laminar boundary layer; with the lower injection rate, the film layer develops slowly and maintains a longer laminar state. As the injection rate increases, the film layer thickens significantly along streamwise direction on the porous wall. After reaching a certain thickness, instability develops, leading to intensified mixing with the incoming boundary layer downstream and the formation of large-scale mixing structures. The position of instability moves upstream with increase in the injection rates, indicating that the higher film injection rates tend to induce boundary layer instability and premature transition. When the injection rate F < 0.2%, the diffusion rate of the seeping gas film into the outer boundary layer is low, and the film maintains a high concentration at the bottom of the boundary layer. With the higher injection rates, the mixing ratio increases and diffuses outward, with a slight decrease in the normal concentration gradient of the film along the wall. For a given injection rate, the diffusion range of the seeping gas film continuously increases but does not exceed 5 mm in thickness. The study shows that the acetone PLIF technology can effectively achieve fine visualization and quantitative analysis of the mixing flow structures of seeping gases within supersonic boundary layers.

Abstract Image

基于丙酮平面激光诱导荧光的超声速边界层渗流气膜混合行为研究
多孔介质渗流是高速车辆中用于减少热量和表面摩擦的主动流动控制方法,但缺乏有效的测量技术来混合渗透气体与来面层。通过在冷却气体中预混约20%的丙酮蒸汽,并采用丙酮平面激光诱导荧光(PLIF)技术,观察了边界层内渗透气膜的流动情况。建立了PLIF图像灰度相对强度与气膜混合率之间的相关性。实验结果表明,在3马赫层流边界层中,渗流气膜层初始保持层流状态;当注入速度较低时,膜层发育缓慢,层状状态持续时间较长。随着注入速度的增加,孔壁上沿流方向的膜层明显增厚。在达到一定厚度后,不稳定发展,导致与下游来面层的混合加剧,形成大规模的混合结构。随着注入速度的增加,不稳定的位置向上游移动,表明较高的注入速度容易引起边界层不稳定和过早转变。当注入速率F <; 0.2%时,渗气膜向外附面层的扩散速率较低,膜在附面层底部保持较高的浓度。随着注射速率的增加,混合比增加并向外扩散,膜沿壁的正常浓度梯度略有降低。在注射速率一定的情况下,渗气膜的扩散范围不断增大,但厚度不超过5mm。研究表明,丙酮PLIF技术可以有效地实现超声速边界层内渗流气体混合流动结构的精细可视化和定量分析。
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来源期刊
Fluid Dynamics
Fluid Dynamics MECHANICS-PHYSICS, FLUIDS & PLASMAS
CiteScore
1.30
自引率
22.20%
发文量
61
审稿时长
6-12 weeks
期刊介绍: Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.
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