后掠压缩斜板进气道进口流场数值研究

对一种后掠压缩斜板进气道(Caret进气道)的进口激波结构、进口流动对管道后部流场的影响进行了数值分析,对进口倒圆修形的影响、激波覆盖面也进行了讨论。数值模拟采用N-S方程和标准k-ε模型加壁面函数方法。计算结果表明:超音速情况下,由于进口存在较强的正激波,进口斜激波强度的不均匀性,对管道内部流动看不出有明显的不利影响;但两压缩面交角处的流动对管道后部流场有较大的影响。      

Analysis of direct operating cost of wide-body passenger aircraft: A parametric study based on Hong Kong

Analysis of the Direct Operating Cost(DOC) of aircraft is an important step towards achieving financially sustainable aviation operations. However, the value of the DOC for different aircraft types and flight scenarios is not widely available. In this study, we perform a systematic analysis of the DOC of every wide-body passenger aircraft currently in production, using the method of the Association of European Airlines(AEA). The elements of the DOC, e.g. financial costs, maintenance costs, and flight costs, are evaluated individually. Several realistic flight scenarios are considered, each with differences in route distance, fuel price, passenger number, and seating arrangement. For each flight scenario, the most cost-efficient aircraft type is identified and evaluated in the context of operations from Hong Kong International Airport. The information provided in this study could be useful to airline operators and policy makers.     

飞机微波着陆模拟器自动计量系统研制CSCD

本文首先简述了MLS模拟器及其计量性能要求,然后对研制的MLS模拟器自动计量系统进行了详细介绍,包括硬件分系统组成及其关键技术,软件分系统架构及其核心流程;最后将自动计量系统应用于多台MLS模拟器的校准/检定。应用表明,MLS模拟器自动计量系统能够解决MLS模拟器计量保障中存在的问题,确保MLS机载设备各项参数准确一致,进而保证了飞行安全。     

A model-scale test on noise from single-stream nozzle exhaust geometries in static conditions

A model-scale test with single-stream nozzle exhaust geometries was carried out at the anechoic chamber of Beihang University in Beijing, China. The spectral characteristics are investigated, and the effects of the following parametric variations are reported in this paper: impact of nozzle operating conditions on spectra; impact of the presence of a plug; and effectiveness of chevron configurations for noise mitigation. The measurement shows that the change of pressure values has more impact on spectra than the change of temperature values. The spectral change due to pressure is shown at all band numbers for unheated conditions whereas it is more pronounced at high-frequency ranges for heated conditions. An impact of the presence of a plug is also clearly observed. The reduction of noise is moderate up to band number of 35, and becomes more significant at higher band numbers. It is observed that chevron nozzles are more efficient at high pressure and temperature values. It is expected that the quantified analysis will be used to develop an empirical model of single jet noise, which will be the baseline for the development of prediction of noise from turbofan engines of high bypass ratios.     

Self-sustained oscillation for compressible cylindrical cavity flows

The presence of a cavity changes the mean and fluctuating pressure distributions. Similarities are observed between a cylindrical cavity and a rectangular cavity for a compressible flow.The type of cavity flow field depends on the diameter-to-depth ratio and the length-to-depth ratio.The feedback loop is responsible for the generation of discrete acoustic tones. In this study, the selfsustained oscillation for a compressible cylindrical cavity flow was investigated experimentally. For open-type cavities, the power spectra show that the strength of resonance depends on the diameterto-depth ratio(4.43–43.0) and the incoming boundary layer thickness-to-depth ratio(0.72–7.0). The effective streamwise length is used as the characteristic length to estimate the Strouhal number. At higher modes, there is a large deviation from Rossiter's formula for rectangular cavities. The gradient-based searching method was used to evaluate the values of the empirical parameters. Less phase lag and a lower convection velocity are observed.     

克服复共线性影响的方法探讨

数据建模是参数估计与精度估计的主要手段，也是实际工程中进行系统故障诊断与修复的主要途径。然而，由于变量之间的复共线性性，严重影响了目前广泛应用于工程实际中的最小二乘方法、主成分估计等方法的收敛性与估计精度，也成为制约各种估计方法实用效果的主要原因。本文详细分析了复共线性影响参数估计的机理，全面讨论了克服复共线性影响的几种常用方法的思想及优劣，并给出了工程实际中在参数估计方面应注意的问题。     

基于级联耦合的大功率测量技术研究CSCD

讨论了采用级联耦合测量技术的大功率测量系统,指出大功率测量条件下引起测量不确定度的因素,搭建了基于该技术的大功率校准系统,减小了系统测量不确定度,实现了功率放大器的高精度校准和测量。     

高超声速气动热数值计算壁面网格准则

首先对高超声速气动热数值模拟中的3种壁面法向网格准则(平均自由程(MFP)、自由来流参数网格雷诺数和壁面参数网格雷诺数准则)进行了分析.随后,提出了壁面参数预估方法,使得壁面参数网格雷诺数和MFP两种准则无需进行试算即可直接预估壁面法向网格尺度.其次,运用提出的壁面参数预估方法结合不同网格准则,在同一实验条件下确定多个壁面法向网格尺度,通过与实验数据对比研究各网格准则确定的壁面法向网格尺度是否满足热环境模拟精度要求,并对提出的壁面参数预估方法进行验证.最后,开展了高超声速二维完全气体及真实气体效应算例、三维钝双锥算例的数值模拟.研究表明,壁面参数预估方法是可靠的;自由来流参数网格雷诺数准则随来流静温变化所确定的网格尺度变化趋势与物理推理相悖;基于壁面参数网格雷诺数和MFP两种准则主要受壁面温度影响,其在同一条件下所确定的网格尺度基本一致,并满足热环境模拟的精度要求.      

基于模态发生器的进气道风扇噪声及声衬降噪实验

为研究发动机进气道风扇噪声特性及声衬降噪效果,使用模态发生器提供声源,采用固定麦克风阵列和旋转扫描耙装置测量进气道内噪声信号,进而利用周向和径向模态分解方法得到声模态幅值,对影响模态分解结果的关键因素进行了研究.对周向模态在时域内进行分解,得到幅值和相位的时变特性.最后完成了2套声衬实验件降噪效果测试.结果表明:模态发...