边界层转捩区声辐射的预报方法研究

对Lighthill剪切应力脉动模型和Liepmann位移厚度脉动模型进行了讨论,在此基础上,本文提出利用Krane偶极子声源模型对Liepmann单极子声源模型进行改进。数值计算结果表明:作为偶极子声源的Lighthill理论剪切应力脉动模型,预报的噪声级偏低;而作为单极子声源的Liepmann模型,预报的噪声级又偏高;本文提出的两种改进模型预报的噪声级则与Lauchle实验值的一致性较好。     

转捩区长度对回转体流噪声的影响

本文通过分析回转体边界层转捩区声辐射的机理,就转捩区长度对回转体转捩区辐射声压谱的影响进行了讨论。结果表明,来流速度和回转体直径是影响回转体转捩区长度、也是影响回轨体转捩区辐射声压谱的主要因素,在来流攻回轨体直径相同时,则回转体形对转捩区长度的影响超主导作用,采用本文的方法所得的理论值与实验值之间的一致性较好。     

回转体流噪声──边界层转捩区的声辐射

基于Liepmann涡声理论,通过引入Lauchle的随机指示器函数,对考虑了声波沿回转体头部曲面传播的声绕射损失的回转体边界层转捩区辐射到头部驻点处的声功率谱进行了分析和估算。结果表明：转捩区的声辐射为单极子声辐射;转捩区的辐射声功率谱的谱峰将随着转捩区长度的减小而向高频迁移;同时,来流速度对其声辐射也有较大的影响．用此方法所得的理论值与实测值之间的一致性较好。     

回转体边界层的高频声辐射

已就回转体边界层声辐射的机理作了分析,并对回转体边界层的辐射声压谱进行了估算。结果表明,回转体边界层声辐射由转捩区和湍流边界层的声辐射组成;在低频段,转换区的声辐射将占主导地位,而在高频段,则湍流边界层的声辐射起主要作用。采用本文的方法所得的理论值与实测值之间的一致性较好。     

展向凹槽及泄流孔对高超声速平板边界层转捩影响的试验研究

针对展向凹槽和泄流孔对高超声速钝平板边界层转捩的影响,在中国空气动力研究与发展中心F2 m激波风洞(FD-14A)开展了试验及初步的计算与理论研究.试验的来流马赫数为6、单位雷诺数为3.3×107/m,平板的前缘半径为1 mm,攻角为–4°.在距平板前缘110 mm处布置三组不同的二维展向凹槽,凹槽的宽度与深度分别为凹槽1(2.5 mm,1 mm)、凹槽2(3.75 mm,1.5 mm)、凹槽3(5 mm,2 mm),同时凹槽1的两端可以打开泄流孔,记为凹槽4,不含凹槽时的光滑平板情况记为凹槽5或平板.采用热流传感器测量了不同情况下平板中心线的热流分布,测量结果显示,光滑平板情况在x≈340 mm处开始转捩,在x≈425 mm处转捩接近完成.凹槽导致平板边界层的转捩位置提前,且随着凹槽宽度及深度的增加,对转捩的促进作用增强,转捩位置向上游移动.凹槽1增加泄流孔后(凹槽4)其热流分布及转捩位置与光滑平板情况基本一致.边界层流动完全转捩为湍流后,各情况下的热流差别较小,表明不同规格的凹槽只影响转捩过程中的热流分布,对转捩完成后的湍流壁面热流影响较小.数值计算(CFD)结果显示,泄流孔导致了被动抽吸,试验结果显示凹槽两端的泄流孔抽吸效应抵消了凹槽对平板中心线边界层转捩的促进作用.采用线性稳定性理论(LST)及最优扰动方法分析了光滑钝平板情况的流动失稳机制.LST结果显示,本文平板流动不存在Mack第一模态、第二模态失稳,因此传统的模态失稳机制无法解释试验中观测到的转捩现象.最优扰动计算显示,平板流动存在较强的非模态失稳,可以定性解释观测到的转捩现象.     

基于Ludwieg管的高超声速边界层转捩实验

高超声速边界层层/湍流转捩是高超声速飞行器气动力和气动热设计中的难点和热点问题.为了降低开展高超声速边界层不稳定性与转捩实验研究的门槛,研究基于Ludwieg管原理设计并建造了一座Mach 6高超声速管风洞,重点对Ludwieg管风洞的启动和运行过程开展了数值模拟,分析了储气段弯管布局对试验段流场的影响;之后,对该高超...     

源于边界层转捩区的单极子声辐射

基于 Lighthill方程和 Green理论,本文对边界层转捩区声辐射机理进行了分析和讨论,并对转捩区内各声源的基本类型作了分类.分析结果表明;边界层转捩区的声辐射由转捩区内处于完全湍流状态的流体流动引起的向边界展外辐射的声场以及另两个附加声场组成;边界层转捩区声源的主要类型为单极子、偶极子和四极子声源;本文的分析为Lauchle模型提供了理论依据,证明了利用Lauchle模型估算转捩区远场声辐射基本准确可靠.     

转捩边界层中流向条纹的新特性

基于边界层转捩后阶段的高精度直接数值模拟结果,发现流向条纹结构的低速条纹的演化过程中存在不连续现象,以及随高速条纹的发展会出现称之为"高速斑"的新特性. 通过详细剖析边界层转捩过程中的复杂涡系结构以及上喷下扫流动现象,证实流向高低速条纹新特性与流场涡系结构的演化过程紧密相关. 关键词： 流向条纹 边界层 转捩 直接数值模拟     

基于POD方法的高超声速边界层转捩判定方法

高超声速边界层转捩是高超声速飞行器设计的关键基础问题之一.为了研究高超声速边界层转捩, 在风洞中, 对平板模型进行了M=5的实验, 在模型中心沿流动方向使用PCB脉动压力传感器对脉动压力时间序列进行采集.文章将本征正交分解(proper orthogonal decomposition,POD)方法引入高超声速脉动压力数据处理中, 发展了单点POD分析方法.经验证, 使用该方法重构数据的均方根(root mean square, RMS)峰值位置可表征转捩位置, 实用性强.      

边界层转捩对风力机气动性能模拟结果的影响

本文采用CFD软件包FINETM/Turbo,选用结合AGS转捩模型的S-A湍流模型,研究边界层转捩对NORD-TANK 500/41型风力机LM19.1叶片三维流场的影响,并与采用-方程S-A和两方程k-ω(SST)模型获得的全湍流计算结果比较.在计算结果与实验数据进行对比的基础上,分析了三维粘性流场的流动细节,探讨了边界层转捩对风力机叶片气动性能和载荷预估的影响,获得了叶片转捩线随风速和沿展向的变化趋势.结果显示边界层转捩使数值计算的叶片性能和载荷增大、边界层分离推迟,为风力机叶片的优化设计提供参考.     

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对等离子体气动激励控制边界层进行了数值仿真。将等离子体气动激励对边界层的作用建模成动量和热量。通过由基于表面放电的二维流体体力模型得到的等离子体气动激励的体力分布函数,得到向边界层注入的动量和热量分布,将动量和热量以源项的形式引入N-S方程求解。研究了等离子体气动激励的强度、激励电极的数目、来流速度的大小以及热量项的大小对等离子体气动激励作用效果的影响,仿真结果与实验一致。     

机体表面湍流边界层噪声特性及预测方法研究

湍流边界层噪声是飞机巡航过程中的主要外部噪声源,对舱内噪声水平的影响尤为重要。因此,对飞机机体表面湍流边界层噪声的研究具有重要意义。本文通过试验获得了某型民机巡航过程中的湍流边界层噪声,试飞工况为3500ft/0.78、3500ft/0.7、2500ft/0.67、1500ft/0.66。对实测数据进行分析,发现湍流边界层噪声与动压、边界层厚度等参数有关。同时,利用计算流体力学的方法得到了飞机机体表面的压力分布,并分析了压力梯度对湍流边界层噪声的影响。最后,基于工程预测方法对湍流边界层噪声进行了预测,对于不存在逆压梯度的区域,预测结果与试验结果吻合较好,仅部分频段存在一定偏差。通过对模型的参数进行优化,改善了预测结果。     

A new boundary method for electromagnetic scattering from inhomogeneous bodies

A new numerical method for scattering from inhomogeneous bodies is presented. In particular, the 2D case of a TM-polarizated incident wave scattered by an infinite cylinder is considered. The scattered field is sought in two different domains. The first one is a bounded region inside the scattering body with an inhomogeneous permittivity ε(x,y). The second one is an unbounded homogeneous region outside the scatterer. An approximate solution for the scattered field inside the scatterer is sought by applying the QTSM technique. The method of discrete sources is used to approximate the scattered field in the unbounded region outside the scattering body. A comparison of the numerical solution with an analytic solution is performed.     

Influence of g-jitter on a laminar boundary layer type diffusion flame

A numerical study was conducted to analyze the effect of g-jitter on micro-gravity flames. A boundary layer laminar diffusion flame was used as a test case. This configuration is commonly used to study flame spread in microgravity, thus it is essential to understand the role of g-jitter in these flames. Furthermore, the role of buoyancy increases with the stream-wise coordinate permitting a systematic study of the impact of acceleration perturbations with a reduced number of experimental results. The evolution of experimental stand-off distances defined during parabolic flights compared well, in a qualitative manner, with numerical simulations, validating the aerodynamic aspects of the model. A systematic study using a sinusoidal function showed that perturbations characterized by high frequencies (>1 Hz) do not affect the flame stand-off distance. This is independent of the amplitude within the range of typical perturbations observed during parabolic flights. Perturbations occurring at lower frequencies significantly affected the flame geometry. Averaging over time through periods much longer than the perturbation cycle did not eventually reveal departure from purely zero-gravity flames. Fuel and oxidizer velocities have opposite effects on the sensitivity of the flames to gravity fluctuations. An increase in oxidizer velocity results in a sensitivity decrease. The influence of the multiple parameters of the problem can qualitatively be combined within a previously reported non-dimensional group. Nevertheless, it cannot account for the influence of frequency.     

Honking noise corrections for traffic noise prediction models in heterogeneous traffic conditions like India

In developing countries like India, the nature of the composition of traffic is heterogeneous. A heterogeneous traffic flow consists of vehicles that have different sizes, speeds, vehicle spacing and operating characteristics. As a result of the widely varying speeds, vehicular dimensions, lack of lane disciplines, honking becomes inevitable. In addition, it changes the urban soundscape of developing countries. In heterogeneous traffic conditions, horn events increase noise level (L_den) by 0.5–13 dB(A) as compared to homogenous traffic conditions. Therefore, the traffic prediction models that are used for homogenous traffic conditions are not applicable in heterogeneous traffic conditions. To increase the accuracy of noise prediction models, in depth understanding of heterogeneous traffic noise is required. Understanding the real traffic noise characteristics requires quantification of some of the basic traffic flow characteristics such as speed, flow, Level Of Service (LOS) and density. In a given roadway, the noise level changes with density and LOS on the road. In this paper, a new factor for horn correction is introduced with respect of Level Of Service (LOS). The horn correction values can be incorporated in traffic noise models such as CRTN, FHWA, and RLS 90, while evaluating heterogeneous traffic conditions.     

The kinetic boundary layer for the Klein-Kramers equation; A new numerical approach

We explore a numerical technique for determining the structure of the kinetic boundary layer of the Klein-Kramers equation for noninteracting Brownian particles in a fluid near a wall that absorbs the Brownian particles. The equation is of interest in the theory of diffusion-controlled reactions and of the coagulation of colloidal suspensions. By numerical simulation of the Langevin equation equivalent to the Klein-Kramers equation we amass statistics of the velocities at the first return to the wall and of the return times for particles injected into the fluid at the wall with given velocities. The data can be used to construct the solutions of the standard problems at an absorbing wall, the Milne and the albedo problem. We confirm and extend earlier results by Burschka and Titulaer, obtained by a variational method vexed by the slow convergence of the underlying eigenfunction expansion. We briefly discuss some further boundary layer problems that can be attacked by exploiting the results reported here.