强迫振动法求解偏航阻尼导数

求解了非定常薄层近似Ｎ－Ｓ方程模拟强迫振动条件下的非定常扰动流场,并在Ｅｔｋｉｎ定义下给出偏航阻尼导数Ｃηγ－Ｃηβｃｏｓα的计算方法和数值积分公式,还给出Ｍａ＝１０,α＝９．８４７°,１９．６８°下的计算结果。     

星载183GHz分谐波混频器的设计

文章采用TERATECH公司研制的肖特基二极管,设计了一种星载183GHz分谐波混频器。长9mm、宽0．42mm的混频器电路被放置在腔体中,包括波导过渡到微带的本振和射频频率匹配部分。仿真结果表明本振功率仅为3mw时,变频损耗在173GHz～193GHz频率范围内小于9dB,变频损耗幅度平坦度小于1dB。     

Unstable unsteady aerodynamic modeling based on least squares support vector machines with general excitation

Common, unsteady aerodynamic modeling methods usually use wind tunnel test data from forced vibration tests to predict stable hysteresis loop. However, these methods ignore the initial unstable process of entering the hysteresis loop that exists in the actual maneuvering process of the aircraft. Here, an excitation input suitable for nonlinear system identification is introduced to model unsteady aerodynamic forces with any motion in the amplitude and frequency ranges based on the Least Squares Support Vector Machines (LS-SVMs). In the selection of the input form, avoiding the use of reduced frequency as a parameter makes the model more universal. After model training is completed, the method is applied to predict the lift coefficient, drag coefficient and pitching moment coefficient of the RAE2822 airfoil, in sine and sweep motions under the conditions of plunging and pitching at Mach number 0.8. The predicted results of the initial unstable process and the final stable process are in close agreement with the Computational Fluid Dynamics (CFD) data, demonstrating the feasibility of the model for nonlinear unsteady aerodynamics modeling and the effectiveness of the input design approach.     

加力燃烧室用锯齿冠状混合器混合特性数值研究

通过三维计算流体动力学(CFD)数值计算,研究了加力燃烧室中三种不同型式的锯齿冠状混合器及环形混合器的掺混性能.结果表明:①锯齿冠状混合器下游形成了流向涡阵列,锯齿布置和倾角对其尺度和强度有较大的影响;②相邻锯齿交错布置的锯齿冠混合器的强化掺混效果最为显著且流动损失相对较低,总压恢复系数相对环形混合器降低在0.2%以内...     

Excitation of electrostatic plasma waves by a moving charged source in a quantum plasma

Within a quantum hydrodynamic model and using the reductive perturbation technique, the nonlinear ion-acoustic wave (IAW) excitations due to a moving charged object in an electron-pair-ion quantum plasma are studied both analytically and numerically. In such quantum plasmas we have derived forced Korteweg-de Vries (fKdV) type equation for finite amplitude nonlinear IAWs. The effect of relevant plasma parameters on solitonic excitations is investigated. Numerical simulation shows the generation of advancing solitons ahead of the forcing term traveling at a faster rate with trailing wakes behind the forcing disturbance. It is found that propagation characteristics of nonlinear excitations are significantly affected by quantum parameter. Additionally, we have pursued our analysis by extending it to account for arbitrary amplitude IA solitons, and derived a system of nonlinear differential equations which are analyzed numerically to study the dynamics. Nonlinear analysis predicts the existence of periodic and quasiperiodic nature of the nonlinear system and reveals that the transition from quasiperiodic to periodic behavior occurs due to the variation of quantum diffraction.     

一种改进的Dolph—Chebyshev方法在阵列天线方向图综合中的应用

通过对传统Chebyshev多项式增加修正因子得到一种修正的Chebyshev多项式，并以此为基础提出了一种新的阵列天线方向图综合方法。与传统Chebyshev综合法相比，该方法可以在保持副瓣电平不变的情况下对主瓣进行任意展宽，待求参数少，综合过程简单，有很强的实用性。     

基于多载频MIMO雷达的Radon-Fourier变换盲速旁瓣抑制

 长时间相干积累方法Radon-Fourier变换(RFT)中盲速旁瓣(BSSL)现象会导致雷达虚警增加、目标检测性能降低。针对BSSL问题,给出了一种基于多输入多输出(MIMO)雷达多载频设计的BSSL抑制方法。首先根据载频与BSSL分布的关系,详细推导了BSSL不交叠的约束条件;然后基于该约束条件给出了具体的载频设计公式。利用设计的载频可得到具有不交叠BSSL的两个RFT输出,通过联合处理这两个RFT输出,可实现BSSL抑制。给出了BSSL抑制性能的评价方法。理论分析和数值实验结果表明,本文算法能够在不降低RFT相干积累性能的同时,有效实现BSSL抑制。     

波瓣混合器流场试验

为了获得加力燃烧室波瓣混合器内的三维流场,采用带热电偶的五孔探针对波瓣混合器内的流场进行了测量.通过试验,得到了波瓣混合器出口不同截面的速度场和温度场,以及波瓣混合器沿流向的热混合效率、总压恢复系数变化规律.试验结果表明:在波瓣混合器尾缘处会产生一对相互逆转的流向涡,流向涡的产生加强了内、外涵气流的对流混合;越靠近波瓣混合器尾缘,内、外涵掺混能力越强,热混合效率增加速度越快,总压恢复系数下降也越快.     

雷达本振相位噪声的数字仿真技术

在现代雷达和通讯系统中 ,本振相位噪声越来越成为决定系统性能的关键因素。分析了本振调相、调幅噪声对相参雷达系统探测性能的影响 ,给出了主杂波环境下雷达发射机调相噪声以及发射机泄漏的调幅噪声的数字仿真模型。在雷达数字仿真系统中使用这些模型 ,可以在各种环境下定量分析微波本振相位噪声对目标探测性能的影响 ,对昂贵的微波系统提出满足总体设计要求的合理指标。     

Oscillations of a viscous liquid in a cylindrical container

The natural damped frequencies of a viscous liquid in a circular cylindrical container are obtained for slipping and anchored contact line at the container wall r = a. In addition the response to translational forced excitation has been determined. The results may also be applied to viscous liquid in a micro-gravity environment, as long as the contact angle of the liquid surface to the cylindrical container wall is in the vicinity of π/2, indicating, that the free liquid surface equilibrium position remains a plane surface. It could be found that there exists in contrast to frictionless liquid a small filling range, in which the liquid performs only an aperiodic motion. The adherence condition at the side wall was replaced by the somewhat weaker condition of an anchored contact line.