赵祎佳, 肖加兵, 刘建华, 等. 激流丝扰动下回转体边界层流动转捩的模态特征[J]. 实验流体力学, 2024, 38(2): 59-67. DOI: 10.11729/syltlx20230108
引用本文: 赵祎佳, 肖加兵, 刘建华, 等. 激流丝扰动下回转体边界层流动转捩的模态特征[J]. 实验流体力学, 2024, 38(2): 59-67. DOI: 10.11729/syltlx20230108
ZHAO Y J, XIAO J B, LIU J H, et al. Mode characteristics of transition flow in the boundary layer of the revolved body under wire spoiler disturbances[J]. Journal of Experiments in Fluid Mechanics, 2024, 38(2): 59-67. DOI: 10.11729/syltlx20230108
Citation: ZHAO Y J, XIAO J B, LIU J H, et al. Mode characteristics of transition flow in the boundary layer of the revolved body under wire spoiler disturbances[J]. Journal of Experiments in Fluid Mechanics, 2024, 38(2): 59-67. DOI: 10.11729/syltlx20230108

激流丝扰动下回转体边界层流动转捩的模态特征

Mode characteristics of transition flow in the boundary layer of the revolved body under wire spoiler disturbances

  • 摘要: 水下航行体首部边界层转捩会产生较强的噪声,严重影响其通信及探测性能。为探明诱发水动力噪声的主要流动结构,本文以SUBOFF缩比模型为研究对象,采用高速水洞实验及大涡模拟方法,获得激流丝扰动下的水下回转体边界层流场。研究发现:边界层内流动在激流丝下游形成分离泡,在分离泡中后部发生转捩,诱发了大量多尺度非定常涡系。采用本征正交分解方法研究了边界层转捩区流向、法向速度脉动及压力脉动的模态特征,发现流向速度脉动的主导模态是分离泡及其沿流向的破碎和下游流向涡,其中分离泡区域流向速度脉动为低于3000 Hz的复合频率,下游流向涡为低于200 Hz的低频结构。法向速度脉动与压力脉动模态特征相似,都呈现出高频、宽频脉动特征,在分离泡附近强度最大。由此推测,分离泡及其破碎是边界层转捩的主要诱因,其诱发的法向速度脉动是产生高/宽频噪声的主要原因,流向速度脉动仅与低频噪声有关。

     

    Abstract: The boundary layer transition of underwater vehicles produces strong noise, which seriously affects the communication and detection performance. In order to explore the main flow structures that induce the flow noise, a SUBOFF model is used as the research object, and the experiment and the large eddy simulation method are used to obtain the boundary layer flow field of the underwater revolved body under wire spoiler disturbances. The flow in the boundary layer first forms a separation bubble downstream of the wire spoiler, and a transition occurs in the posterior part of the separation bubble, which induces a large number of multi-scale unsteady vortices. Furthermore, based on the proper orthogonal decomposition method, the mode characteristics of the streamwise and normal velocity pulsation as well as the pressure pulsation in the boundary layer transition zone are studied. It is found that the dominant mode of the streamwise velocity pulsation is the separation bubble and its breakdown along the streamwise direction as well as streamwise vortex downstream. The streamwise direction pulsation in the separated bubble area has a composite frequency of < 3000 Hz, and in the downstream vortex region has a low-frequency structure of < 200 Hz. The mode characteristics of the normal velocity pulsation and pressure pulsation are similar. They are both high-frequency, broad-frequency modal structures with the greatest intensity near the separation bubble. It is inferred that the separation bubble and its breakdown are the main inducements of boundary layer transition, the induced normal velocity pulsation is the main source of high/broadband noise, and the streamwise velocity pulsation is only related to low frequency noise.

     

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