考虑螺旋桨滑流影响的机翼气动优化设计

涡桨飞机的机翼、短舱等部件在滑流作用下周围的流场特性与无滑流状态下截然不同。所以,应该在涡桨飞机的机翼气动设计过程中考虑螺旋桨滑流的影响,从而使得机翼在真实飞行时滑流作用下表现出更好的气动特性。采用基于雷诺平均Navier-Stokes方程的多重参考坐标系(MRF)方法对螺旋桨滑流进行高精度准定常数值模拟,通过自由变形(FFD)技术实现螺旋桨飞机机翼的参数化构建,应用径向基函数(RBF)插值的动网格技术进行网格自动生成,获得样本机翼在滑流影响下的气动数据后,建立目标函数和状态函数的Kriging代理模型,结合随机权重粒子群优化(PSO)算法、Kriging代理模型和对应的EI(Expected Improvement)函数加点准则进行加样本点以及代理模型重建,从而建立滑流影响下机翼气动优化设计系统。使用该系统对某型螺旋桨飞机进行了滑流影响下的优化设计,结果表明,优化后的构型机翼和短舱在巡航状态下减阻达3.98counts,升阻比提高了3.325%。因此,建立的考虑滑流影响下的机翼优化设计方法是可行的。     

结构因素对离心通风器性能影响的数值研究

在高转速下,航空发动机离心通风器内腔存在强烈的湍流流动,而稳定工作后通风器内腔中漩涡呈周期性产生和淹灭。小尺寸颗粒受流体微团湍流随机脉动的影响,产生相对于平均流的随机脉动运动。为了研究通风孔偏心距和辐板顶圆半径对通风器性能的影响,采用离散相模型(DPM)模拟通风器内颗粒的运动轨迹。并应用随机游走(DRW)模型模拟连续相湍流瞬时速度脉动对颗粒轨迹的影响,采用随机涡寿命模型确定随机追踪模型的积分时间。结果表明:辐板顶圆半径的增大有助于提高通风器的分离效率,同时也增大了腔内流通阻力;通风孔偏心距对减小通风阻力的作用明显,但降低了离心通风器的分离效率。     

基于RBF神经网络的控制电器元件故障诊断

针对控制电器元件故障征兆与故障类型之间的非线性映射关系,提出了基于径向基函数神经网络RBFNN(Radial Basis Function Neural Network)的控制电器元件故障诊断方法.在分析控制电器元件故障机理和失效形式的基础上,提取出描述故障类型的典型故障特征矢量.给出在获得足够多故障信息的情况下,运用RBFNN进行故障诊断的模型及整个故障诊断算法的实现过程.为了验证故障诊断模型的有效性和合理性,利用训练好的RBFNN对故障特征矢量进行识别.仿真结果表明,RBFNN能克服诊断过程中容易陷入局部极小的缺点,并能满足故障诊断的快速性和准确性要求.      

改进免疫算法在函数优化中的应用

在对已有克隆选择算法的抗体行为特征分析的基础上,提出了一种新的偏心动态免疫克隆算法(EDICA,Eccentric Dynamic Immune Clone Algorithm).利用进化过程中子代抗体比父代抗体更靠近最优解的启发性信息,提出偏心变异策略,使抗体更快地靠近最优解域.引入控制因子,通过动态调整变异搜索半径的方法,在进化初期加大步长以加快搜索速度,而在后期减小搜索粒度以提高优化精度.采用超球体混沌变异策略以克服各向异性的不利影响并提高全局搜索能力.实验结果表明:EDICA不仅能够准确地找到静态函数的多个最优点,而且还能以较高的精度锁定和跟踪动态函数的最优点.     

Time series analysis of active galactic nuclei: The case of Arp 102B, 3C 390.3, NGC 5548 and NGC 4051

We used the Z-transformed Discrete Correlation Function (ZDCF) and the Stochastic Process Estimation for AGN Reverberation (SPEAR) methods for the time series analysis of the continuum and the Hα$\alpha$ and Hβ$\beta$ line fluxes of a sample of well known type 1 active galactic nuclei (AGNs): Arp 102B, 3C 390.3, NGC 5548, and NGC 4051, where the first two objects are showing double-peaked emission line profiles. The aim of this work is to compare the time lag measurements from these two methods, and check if there is a connection with other emission line properties. We found that the obtained time lags from Hβ are larger than those derived from the Hα analysis for Arp 102B, 3C 390.3 and NGC 5548. This may indicate that the Hβ   line originates at larger radii in these objects. Moreover, we found that the ZDCF and SPEAR time lags are highly correlated (r∼0.87$r\sim 0.87$), and that the error ranges of both ZDCF and SPEAR time lags are correlated with the FWHM of used emission lines (r∼0.7$r\sim 0.7$). This increases the uncertainty of the black hole mass estimates using the virial theorem for AGNs with broader lines.     

Bottom side profiles for two close stations at the southern crest of the EIA: Differences and comparison with IRI-2012 and NeQuick2 for low and high solar activity

Bottom side electron density profiles for two stations at the southern crest of the Equatorial Ionization Anomaly (EIA), São José dos Campos (23.1°S, 314.5°E, dip latitude 19.8°S; Brazil) and Tucumán (26.9°S, 294.6°E, dip latitude 14.0°S; Argentina), located at similar latitude and separated by only 20° in longitude, have been compared during equinoctial, winter and summer months under low (year 2008, minimum of the solar cycle 23/24) and high solar activity (years 2013–2014, maximum of the solar cycle 24) conditions. An analysis of parameters describing the bottom side part of the electron density profile, namely the peak electron density NmF2, the height hmF2 at which it is reached, the thickness parameter B₀ and the shape parameter B₁, is carried out. Further, a comparison of bottom side profiles and F-layer parameters with the corresponding outputs of IRI-2012 and NeQuick2 models is also reported. The variations of NmF2 at both stations reveal the absence of semi-annual anomaly for low solar activity (LSA), evidencing the anomalous activity of the last solar minimum, while those related to hmF2 show an uplift of the ionosphere for high solar activity (HSA). As expected, the EIA is particularly visible at both stations during equinox for HSA, when its strength is at maximum in the South American sector. Despite the similar latitude of the two stations upon the southern crest of the EIA, the anomaly effect is more pronounced at Tucumán than at São José dos Campos. The differences encountered between these very close stations suggest that in this sector relevant longitudinal-dependent variations could occur, with the longitudinal gradient of the Equatorial Electrojet that plays a key role to explain such differences together with the 5.8° separation in dip latitude between the two ionosondes. Furthermore at Tucumán, the daily peak value of NmF2 around 21:00 LT during equinox for HSA is in temporal coincidence with an impulsive enhancement of hmF2, showing a kind of “elastic rebound” under the action of the EIA. IRI-2012 and NeQuick2 bottom side profiles show significant deviations from ionosonde observations. In particular, both models provide a clear underestimation of the EIA strength at both stations, with more pronounced differences for Tucumán. Large discrepancies are obtained for the parameter hmF2 for HSA during daytime at São José dos Campos, where clear underestimations made by both models are observed. The shape parameter B₀ is quite well described by the IRI-2012 model, with very good agreement in particular during equinox for both stations for both LSA and HSA. On the contrary, the two models show poor agreements with ionosonde data concerning the shape parameter B₁.     

一类分数阶薛定谔方程孤立解的对称性研究

在有界环形区域上,研究了一类分数阶薛定谔方程孤立解的对称性问题。首先将分数阶薛定谔方程转化为包含Bessel位势和Riesz位势的积分方程组,然后利用移动平面法和Hardy-Littlewood-Sobolev不等式,证明了当方程边值为常数时,环形区域必为同心球,方程正解是径向对称的,且随着到对称点的距离增大而单调递减。     

弹道导弹动态全极化一维像仿真研究

研究了弹道导弹动态全极化一维像的仿真方法,可以为雷达目标检测、识别算法的研究提供基础。对弹道导弹的弹道和运动特性进行了建模,通过对弹头缩比模型静态测量数据进行插值,可以获得任意时刻、任意姿态下弹头的全极化一维距离像;比较了典型宽带雷达体制的信号形式,推导了它们之间的仿真参数转换关系。在计算机上进行了仿真实验,对仿真结果的分析表明本文提出的仿真方法是切实可行的。     

相机保护罐玻璃对摄影测量精度的影响规律分析与误差补偿

文章通过统计相机镜头处加玻璃前后点位的位移分布规律,选择合适数学模型,将玻璃对测量精度造成的影响减弱。现已完成相机保护罐玻璃对测量精度影响的实验,实验表明:加玻璃后像点坐标变化量最大约为5μm,该变化量的分布与镜头畸变规律相似。最后将其影响划归为径向畸变模型,并通过实验证明该方法能够有效减弱玻璃对测量精度影响。     

转子径距比对燃料电池气体循环泵性能的影响

为了揭示径距比对凸轮式气体循环泵的气动性能的影响规律，通过坐标变换推导了3叶的圆弧-渐开线-圆弧转子型线方程，建立6种不同径距比的气体循环泵模型进行对比分析。采用重整化k-ε（RNG k-ε）湍流模型对转子腔内部进行三维非定常数值计算，结合动网格技术分析转子径距比对气体循环泵流量特性、转子腔速度分布的影响规律，并与试验结果进行对比。结果表明：转子径距比对气体循环泵性能影响较为明显，随着转子径距比由1.34增大到1.45，泵出口平均流量与瞬时流量脉动呈上升趋势，且在1.38~1.40时变化较为明显，平均流量增大了0.001 833 m³/s（15.8%）；转子径距比在1.38~1.40时，转子受力较好，对转子径向激励力分量F_x的抑制较为明显，对转子径向激励力分量F_y的影响不显著；随径距比变化，转子腔内涡量分布变化较为明显，转子径距比在1.40时，转子腔内涡量分布较小，有效抑制了气体回流。