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841.
风扇/压气机转子、静子干涉噪声的预测方法   总被引:1,自引:1,他引:1  
 本文采用管道声学模型计算了由转子尾迹与静子相互作用产生的干涉声音的大小。分析了转子、静子相对距离的变化对声音大小的影响,并与试验结果进行了对比。  相似文献   
842.
直接数字合成技术的应用   总被引:3,自引:0,他引:3  
介绍直接数字合成(DDS)技术的原理和当前发展水平。运用该技术改进设计了某型号作战系统中的多普勒频率  相似文献   
843.
光纤加速度计强度噪声的研究   总被引:1,自引:0,他引:1  
杨革文 《上海航天》2003,20(5):29-32,49
对光纤加速度计系统中由激光光源51入的具有1/f特性的强度噪声进行了分析,阐速了强度噪声产生的机理及其对系统性能的影响,并提出相应的解决方案。实验结果与分析所得结论基本吻合。该方法对提高光纤加速度计低频段灵敏度有重要的参考价值。  相似文献   
844.
对于现代先进涡扇发动机,占比越来越大的风扇/压气机宽频噪声成为亟需解决的问题。基于三维风扇声源模型,开展了湍流输入参数对宽频噪声预测影响的研究。结果表明:后传声功率级比前传声功率级普遍高5 dB左右;当湍流参数增大时,也会较大幅度改变前传和后传的声功率级,但对频谱形状影响较小;声功率级随湍流积分尺度增大而减小,随背景湍流速度、中心线湍流速度、湍流宽度增大而增大,其中背景湍流速度对宽频噪声影响最大。发现湍流参数通过作用于上洗速度谱来影响宽频噪声预测结果。   相似文献   
845.
During振子临界态相变对弱信号检测研究非常重要,文中研究During临界状态的性能。介绍了随机微分方程理论关于噪声对系统周期态影响的分析;然后为克服存在的过渡过程,建立改进的系统仿真模型。通过仿真试验分析During振子临界态的性能,混沌态与大尺度周期态表现的性能差别深化了对混沌现象的认识;重点研究受噪声干扰的系统运动状态变化情况,得出系统运动越接近临界态越对噪声敏感,噪声越强周期态运动容易再次跃迁回混沌态,说明随机微分方程理论分析临界状态结果不正确;实验结果还表明,噪声是在某些特定条件下导致处于临界大尺度周期态运动的系统发生突变分又跃迁回混沌状态,值得进一步深入研究。  相似文献   
846.
地震计量用标准振动台技术总结   总被引:2,自引:0,他引:2  
本文深入探讨了地震计量用标准振动台研制中台面的失真度、信噪比、横向运动三个主要技术难题及其相应的改进对策。文中的论述对于普通标准振动台的设计也具有一般的指导意义。  相似文献   
847.
Precise clock products are typically interpolated based on the sampling interval of the observational data when they are used for in precise point positioning. However, due to the occurrence of white noise in atomic clocks, a residual component of such noise will inevitable reside within the observations when clock errors are interpolated, and such noise will affect the resolution of the positioning results. In this paper, which is based on a twenty-one-week analysis of the atomic clock noise characteristics of numerous satellites, a new stochastic observation model that considers satellite clock interpolation errors is proposed. First, the systematic error of each satellite in the IGR clock product was extracted using a wavelet de-noising method to obtain the empirical characteristics of atomic clock noise within each clock product. Then, based on those empirical characteristics, a stochastic observation model was structured that considered the satellite clock interpolation errors. Subsequently, the IGR and IGS clock products at different time intervals were used for experimental validation. A verification using 179 stations worldwide from the IGS showed that, compared with the conventional model, the convergence times using the stochastic model proposed in this study were respectively shortened by 4.8% and 4.0% when the IGR and IGS 300-s-interval clock products were used and by 19.1% and 19.4% when the 900-s-interval clock products were used. Furthermore, the disturbances during the initial phase of the calculation were also effectively improved.  相似文献   
848.
文章基于传统Sigma滤波器,提出了一种新的SAR图像滤波方法。首先,分析指出传统Sigma滤波器处理复合噪声和保持弱边缘的能力较弱的缺点。然后,改进Sigma滤波器的δ-条件,使之更加适应复合噪声分布条件下的SAR图像滤波。提出了灰度中心偏移的Sigma滤波(GCOSF),增强Sigma滤波器保持弱边缘的能力。在GC...  相似文献   
849.
    
This paper evaluates the impact of residual acceleration noise on the estimation of the Earth’s time-varying gravity field for future low-low satellite-to-satellite tracking missions. The goal is to determine the maximum level of residual acceleration noise that does not adversely affect the estimation error. The Gravity Recovery And Climate Experiment (GRACE) has provided monthly average gravity field solutions in spherical harmonic coefficients for more than a decade. It provides information about land and ocean mass variations with a spatial resolution of ~350?km and with an accuracy within 2?cm throughout the entire Earth. GRACE Follow-on was launched in May 2018 to advance the work of GRACE and to test a new laser ranging interferometer, which measures the range between the two satellites with higher precision than the K-Band ranging system used in GRACE. Moreover, there have been simulation studies that show, an additional pair of satellites in an inclined orbit increases the sampling frequency and reduces temporal aliasing errors. Given the fact that future missions will likely continue to use the low-low satellite-to-satellite tracking formation with laser ranging interferometry, it is expected that the residual acceleration noise will become one of the largest error contributor for the time-variable gravity field solution. We evaluate three different levels of residual acceleration noise based on demonstrated drag-free systems to find a suitable drag-free performance target for upcoming geodesy missions. We analyze both a single collinear polar pair and the optimal double collinear pair of drag-free satellites and assume the use of a laser ranging interferometer. A partitioned best linear unbiased estimator that was developed, incorporating several novel features from the ground up is used to compute the solutions in terms of spherical harmonics. It was found that the suitable residual acceleration noise level is around 2?×?10?12?ms?2?Hz?1/2. Decreasing the acceleration noise below this level did not result in more accurate gravity field solutions for the chosen mission architecture.  相似文献   
850.
Numerical analysis of broadband noise reduction with wavy leading edge   总被引:3,自引:2,他引:3  
Large Eddy Simulation(LES) is performed to investigate the airfoil broadband noise reduction with wavy leading edge under anisotropic incoming turbulence. The anisotropic incoming turbulence is generated by a rod with a diameter of 10 mm. The incoming flow velocity is 40 m/s and the corresponding Reynolds numbers based on airfoil chord and rod diameter are about 397000 and 26000, respectively. The far-field acoustic field is predicted using an acoustic analogy method which has been validated by the experiment. A straight leading edge airfoil and a wavy leading edge airfoil are simulated. The results show that wavy leading edge increases the airfoil lift and drag whereas the lift and drag fluctuations are substantially reduced. In addition, wavy leading edge can significantly change the flow pattern around the leading edge and a pair of counter-rotating streamwise vortices stemming from each wavy leading edge peak are observed.An averaged noise reduction of 9.5 dB is observed with the wavy leading edge at the azimuthal angle of 90°. Moreover, the wavy leading edge can mitigate noise radiation at all the azimuthal angles without significantly changing the noise directivity. The underlying noise reduction mechanisms are then analyzed in detail.  相似文献   
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