Numerical Study on the Duct Acoustic Mode Control of Turbine Interaction Noise with Serrated Configurations

Turbine noise would be one of the dominant noise sources especially in future UHBR (Ultra High Bypass-Ratio) aeroengine, but its currently far from being studied enough. Acoustic mode is crucial for duct propagation but little study about the relation between serration and mode. Thus, taking axial single-turbine test bench NPU-Turb as object, the effect of Stator with Serrated Trailing-edge (Bionic S) and Rotor with Serrated Leading-edge (Bionic R) on duct acoustic modes of turbine turbulence interac-tion noise were studied in detail using DDES/AA hybrid model validated by acoustic experiment of NPU-Turb. Serval conclusions can be made here. First, for broadband noise, the effect of serrations on duct modes (increased or reduced of PWLmn) with the increasing frequency is more prominent. Second, the changing trend of ?PWLmn is something like Chinese character “人” with circumferential mode m and alternating with radial mode. Such distribution is more obvious at higher frequency. More theoretical and mechanistic research work needs to be carried out in depth in the future. .

MATCH-MODE METHOD AND ITS NUMERICAL SIMULATION FOR ROTOR-STATOR INTERACTION SOURCE MODES AND PROPAGATION MODES IN AN ANNULAR DUCT WITH MULTI-TREATMENTS

The suppressing design of the engine nacelle in an aircraft can benefit from the development of the prediction system for the sound fields in engine ducts which includes the prediction of the source generation and that of sound propagation in ducts. First, the acoustic match mode principle between the source modes of rotor stator interaction noise and the propagation modes is presented in this paper. Second, by utilizing this principle, the theoretical prediction method for rotor stator interaction noise generation and its propagation and attenuation in an annular duct with multi treatments is developed. That means that the prediction of sound propagation and attenuation in the segmented ducts might no longer completely depend on the in duct mode measurements, and the investigation on the sound propagation and attenuation in ducts can be accomplished not only by acoustic mode measurement, but also by making use of the source prediction to determine the source modes excited by rotor stator interaction. The effects of fan speed, blade/vane numbers, axial spacing between rotor and stator on the in duct sound attenuation and generated sound power level before and after ducts (also including the sound power level of blade passing frequency and its harmonics at the inlet of ducts) have been numerically calculated by using this prediction method. The reliability of this prediction method is verified by reasonable agreement between the predicted results with measured results in references. By analyzing the results of calculating cases, some reference criteria are provided for the engineering design of the suppressing engine nacelle.

Numerical simulation of radiated noise during combustion of energetic materials in a closed bomb

In this study,based on a closed bomb test combined with computational fluid dynamics,a structural finite element method,and an acoustic boundary element method,a fluid-solid acoustic one-way coupling calculation model is established for the combustion process of energetic materials in a closed bomb,and the effectiveness of the model is verified by experiments.It is found that the maximum peak sound pressure increases exponentially with an increase in loading doses or gas pressure.However,a change in the combustion coefficient of the energetic materials has little effect on the noise generated during the combustion process in the closed bomb.When the combustion coefficient is reduced by a multiple of 16,the maximum transient sound pressure is reduced by 1.79 dB,and the sound pressure level in the frequency band is reduced by 1.75 dB.With an increase in shell thickness,the combustion noise of the energetic materials in the closed bomb decreases,and the reduction range of the combustion noise increases with the increase in shell thickness.

Expectation-maximization (EM) Algorithm Based on IMM Filtering with Adaptive Noise Covariance

A novel method under the interactive multiple model (IMM) filtering framework is presented in this paper, in which the expectation-maximization (EM) algorithm is used to identify the process noise covariance Q online. For the existing IMM filtering theory, the matrix Q is determined by means of design experience, but Q is actually changed with the state of the maneuvering target. Meanwhile it is severely influenced by the environment around the target, i.e., it is a variable of time. Therefore, the experiential covariance Q can not represent the influence of state noise in the maneuvering process exactly. Firstly, it is assumed that the evolved state and the initial conditions of the system can be modeled by using Gaussian distribution, although the dynamic system is of a nonlinear measurement equation, and furthermore the EM algorithm based on IMM filtering with the Q identification online is proposed. Secondly, the truncated error analysis is performed. Finally, the Monte Carlo simulation results are given to show that the proposed algorithm outperforms the existing algorithms and the tracking precision for the maneuvering targets is improved efficiently.

Flow-induced Noise and Vibration Analysis of a Piping Elbow with/without a Guide Vane

指南翼的效果安装了非常近从 1.70 汦潯敤 ? 楷桴在雷纳兹数字的范围在导致流动的噪音和颤动上被调查吗？

Interaction tonal noise generated by contra-rotating open rotors

Fast and accurate prediction of sound radiation of Contra-Rotating Open Rotors(CRORs)is an essential element of design methods of low-noise open rotor propulsion systems.In the present work,a previous frequency-domain model is extended to predict CROR noise.It builds explicitly the relationship between harmonic loadings and corresponding tonal noise,by which the influential parameters to noise generation can be clearly understood.The real distribu-tions of steady and unsteady blade loadings are calculated by the Nonlinear Harmonic(NLH)method.In the present hybrid approach,both the CFD and acoustic modules are solved in the fre-quency domain.To assess the accuracy of the developed method,the loading noise of a CROR is calculated and compared against results by using the time-domain FW-H module of NUMECA.The predicted sound directivities by the two methods are in good agreements.The present acoustic model in the frequency domain is proven to be accurate and have high efficiency in far-field noise prediction and data processing.Furthermore,the characteristics of the CROR interaction tonal noise are analyzed and discussed.

Experimental and numerical investigation on sound generation from airfoil-flow interaction

Aerodynamic noise due to interaction between incoming turbulence and rotating blades is an important component in the wind turbine noise. The rod-airfoil configuration is used to investigate the interactive phenomenon experimentally and nu- merically. Distribution of unsteady pressure on the airfoil surface is measured for different rod positions and airfoil attack angles. Two National Advisory Committee for Aeronatics （NACA） airfoils, NACA0012 and NACA0018, and two wind turbine airfoils, S809 and S825 are investigated. In addition, for low angles of attack, the flow field around the airfoil＇s leading edge is investigated with the particle image velocimetry （PIV）. The experimental results indicate that unsteady pressure disturbances on the airfoil surface are related to the rod vortex shedding. Meanwhile, the interaction flow field of the rod and NACA0012 airfoil is simulated with the unsteady Reynolds averaged Navier-Stokes method （URANS）, and the obtained pressure spectra are compared with the experimental results.

Hydrodynamic Interactions Introduce Differences in the Behaviour of a Ratchet Dimer Brownian Motor

We use the Brownian dynamics with hydrodynamic interactions simulation in order to describe the movement of an elastically coupled dimer Brownian motor in a ratchet potential. The only external forces considered in our system were the load, the random thermal noise and an unbiased thermal fluctuation. We observe differences in the dynamic behaviour if hydrodynamic interactions are considered as compared with the case without them. In conclusion, hydrodynamic interactions influence substantially the dynamics of a ratchet dimer Brownian motor;consequently they have to be considered in any theory where the molecular motors are in a liquid medium.

The effects of initial perturbation to mixing-layer noise

The far-field noise radiated from mixing layers is determined by the near-field flow dynamics which is sensitive to the initial perturbation of instability introduced physically or numerically.This study focuses on the effects of the phase delay in two initial perturbations,one at the fundamental wave number and the other at its subharmonic both calculated from linear instability analysis,on the sound generation in mixing layers.When different phase delaysφ_1 changing from zero to 2πis applied on the fundamental mode,we observe different vortex merging processes（e.g.vortex pairing or tearing）.The strong nonlinear interaction in the merging process generates most of the noise from mixing layers.There shows a pattern in a period of 2πfor the response of far-field sound to the change ofφ_1.Similar effects on the dynamics and acoustics can be achieved by adding different phase delaysφ_2 to the subharmonic mode instead,however,the response repeats in a period of onlyπforφ_2.The effects of the combination of different phase delays to other parameters,including the amplitude and wave number for each perturbations,are also investigated.All the results indicate a critical role of nonlinearity in the sound generation mechanism of mixing layers.

基于固-气-液耦合的气垫船水下辐射噪声数值分析

气垫船水下声辐射是复杂的船体结构-气垫-周围水体三类介质声振耦合过程,其声传递特性是气垫船声学分析中的难点。本文以某全垫升气垫船为研究对象,结合声固耦合有限元法与解析法,探究气垫船水下辐射噪声传递特性。通过建立固-气-液声固耦合有限元模型,计算机械激励与垫升风机声激励,并以试验固有频率修正数值模型;通过声透射解析公式计算空气螺旋桨、燃气轮机等设备声激励辐射的水下噪声。采用距离左、右舷1 m处线上各点的总声压级作为评价指标。结果表明:气垫船水下辐射噪声为宽带噪声;有限元法计算的水下辐射噪声在低频时集中分布于气垫-周围水体耦合面附近,随着频率的升高,水下噪声增大并逐渐呈不规则干涉状分布;空气螺旋桨等声激励直接辐射水下噪声主要为近场低频噪声,在设备声激励辐射范围内声压平均占比约为40%。本文揭示的水下辐射噪声传递特性对气垫船减振降噪具有重要指导意义。

基于流固耦合的压缩机吸气阀组气动噪声研究

往复式压缩机吸气阀组工作过程存在明显的流固耦合现象,现有的固定阀片开度的数值仿真模型大多没有考虑流固耦合现象,而考虑流固耦合现象的数值仿真模型由于忽略了活塞和阀板的作用难以获取足够的声源信息。文章建立考虑活塞和阀板作用的流固耦合数值仿真模型,并与其他模型获得的运动、流场和声场特性进行对比,结果表明:所建立的流固耦合模型能够更准确地描述吸气阀组的工作过程,获得更丰富的声源信息;基于该流固耦合数值仿真模型开展通流截面参数对吸气阀组气动噪声的影响分析,并优化设计了截面参数。

考虑滚动噪声的地铁波磨打磨限值评估方法

钢轨打磨能有效抑制波磨的发展,目前的打磨限值制定标准主要以车辆运行平稳性和行车安全性为依据,对影响环境线路的轮轨滚动噪声重视不足。为了获取服役条件下轮轨滚动噪声约束的地铁波磨打磨限值,根据对某地铁线路噪声段波磨情况的调查,建立了地铁波磨打磨限值综合评估模型。模型中将连续谐波模拟钢轨波磨作为系统输入,根据车辆-轨道耦合动力学理论以及轮轨接触关系确定轮轨动作用力和轮轨表面粗糙度之间的关系,分析获取了车辆-轨道耦合系统的振动响应和轮轨滚动噪声,指出了轮轨动作用力、轮重减载率和轮轨滚动噪声声压级3个指标对地铁线路钢轨波磨打磨限值的影响,进而形成了融合轮轨滚动噪声的地铁波磨打磨限值评估方法。结果表明:考虑轮轨滚动噪声影响的钢轨波磨打磨限值评估,不仅满足车辆运行平稳性和行车安全性的要求,而且保证地铁沿线噪声处于合理范围;基于轮轨滚动噪声对钢轨波磨最为敏感的特性,综合评估地铁波磨打磨限值,提高了载重变化时的车辆运行平稳性。

基于变分贝叶斯算法的多模型车载组合导航算法

在行车过程中强机动引起全球卫星导航系统(GNSS)量测噪声产生野值,表现出厚尾特性导致常规状态估计精度下降的问题,为此提出一种基于变分贝叶斯的SINS/GNSS组合导航信息融合方法。构建车载组合导航系统模型,采用Student’s t分布对量测异常情况下噪声建模,并用变分贝叶斯的方法对系统状态和隐变量进行求解,实现对模型参数的后验估计。针对城市行车存在GNSS测量失效的问题,利用交互式多模型算法实现了GNSS量测中断情况下的SINS/GNSS和SINS/OD子系统的动态交互融合。通过跑车实验进行验证,实验结果表明,所提算法可有效抑制GNSS量测野值噪声对SINS/GNSS/OD组合导航系统的影响,与传统交互式多模型算法相比,具有较高的精度和鲁棒性。

基于流固耦合的AUV伴流对螺旋桨性能影响

自主式水下航行器(Autonomous Underwater Vehicle,AUV)螺旋桨的运转通常是在非均匀流场中,其中以AUV航行时产生的尾部伴流为主。为了分析尾部伴流对螺旋桨水动力及噪声的影响,首先利用P 4 119螺旋桨验证双向流固耦合数值模拟的可行性、准确性,其次建立AUV与B型图谱桨耦合模型,对比2种工况下螺旋桨动力性能与无空化噪声分布情况。结果表明,在AUV尾部不均匀的来流影响下,螺旋桨所需提供的推力和转矩有所提高,此增幅在最高时分别可以达到83.77%和50.50%;相较于1倍叶频时伴流对螺旋桨噪声的微弱影响,2倍和3倍叶频时螺旋桨噪声在各个监测点的声压级相较均匀来流衰减了20~50 dB,并且导致2倍叶频时螺旋桨噪声的分布呈现无规则形。

基于语音增强的改进型英语课堂交互系统的研究

针对复杂噪声环境下英语课堂交互系统语音识别性能下降的问题,文章提出将双路Transformer语音增强网络作为降噪模块引入该系统,通过对噪声环境下的英语语音数据进行降噪增强,提升英语交互系统的语音识别准确性。搭建实验环境对改进的方式进行验证,实验结果表明,改进后的方式能够有效提升复杂噪声环境下英语课堂交互系统的语音识别准确性。

基于流固耦合的风荷载作用下声屏障强度分析

为了解道路上风荷载作用下声屏障周围的流场、所受风压、结构强度等情况,采用流固耦合分析方法对声屏障进行强度分析。采用单向流固耦合技术,首先建立声屏障流场模型,采用有限体积法求解稳态不可压流体湍流方程,分析流场计算结果,并提取流场中声屏障表面的风压数据;然后建立声屏障有限元模型,依次施加重力、风压进行静力计算,对声屏障强度进行校核。结果表明:受验模型的声屏障立柱、基础连接、螺栓均满足强度要求,并且采用单向流固耦合分析方法对声屏障进行风荷载条件下的强度分析具有可行性。

基于沥青路面纹理解构的轮胎/路面噪声预测方法研究

轮胎/路面噪声TPIN已成为城市环境噪声污染的重要组成部分,路面纹理是TPIN的重要影响因素。采用三维激光扫描技术获得路面点云数据,建立路面纹理三维模型,根据灰度共生矩阵(GLCM)、分形理论(FD)和功率谱密度理论(PSD)计算整体、宏观和微观纹理指标对路面纹理进行解构,建立基于纹理指标的TPIN线性回归和随机森林预测模型。结果表明:1)3种理论所计算的纹理指标可有效解构纹理,与TPIN有较好的相关性;2)车速在60 km/h时,TPIN与微观纹理的相关性更强,路面关键波长与噪声测试的轮胎波长有关;3)随机森林的预测精度高于单因素预测模型,最佳预测精度为R^(2)=0.9885,MSE=0.0004,预测效果较好。因此,可将路面纹理作为有效评价TPIN的方法。

直立式混凝土落地声屏障振动放大效应

以普速铁路路侧落地安装直立式混凝土声屏障为研究对象,利用原位试验方法研究了列车运行下屏障板水平及竖向加速度时程和频谱特征,结合悬臂板理论模态分析了屏障板相对其基础的振动放大效应及机理。结果表明,钢轨-轨枕-道床-声屏障基础振动递减,屏障板较其基础加速度平均放大2倍,振级平均增大6 dB,道床和基础竖向振动卓越频率为63.5 Hz,水平向放大显著频段为6~8 Hz和40~50 Hz,竖向放大显著频率为63.5 Hz和160 Hz。理论模态分析显示,屏障板水平向前2阶自振频率为7 Hz和46 Hz,竖向1阶自振频率为170 Hz,说明水平放大效应与其前2阶自振频率相关,竖向放大效应与其1阶自振频率和基础激励频率相关。将屏障板振动响应估算简化为地基土-声屏障动力相互作用耦合振动模型,以考虑其受地基激励强迫振动和自由振动双重影响是合理可行的。

Effects of Diffuser Vane Geometry on Interaction Noise Generated from a Centrifugal Compressor

相互作用音调噪音的特征与 vaned 从一台离心的压缩机放射了更弥漫被实验讨论，包括用油电影方法的可视化技术。研究注意对是的更弥漫的翼的前缘几何学被给予深深地与相互作用音调噪音的产生机制有关。散发压缩机的噪音能被在压力上升系数与某衰落一起将一些清理放在中心和更弥漫的墙的笼罩表面被几分贝减少。自从结果被第二等的流动被流动冲击并且也在更弥漫的段落以内引起的衰落，不从表演和噪音水平毁损的更弥漫的翼几何学的几种新类型为实验被开发并且利用。介绍的更弥漫的翼几何学将为更弥漫的翼设计为一些提供基本指南。关键词离心的压缩机 - vaned 更弥漫 - 相互作用噪音 - 噪音减小 CLC 数字 TK474.