高功率微波大气击穿区域分布

大气击穿是高功率微波(HPM)大气传输研究最主要的内容。一方面高功率微波辐射天线近场以振荡场形式存在,在某些局部点形成场强的峰值分布,导致天线近场击穿、天线口径面介质击穿等一系列复杂的问题;另一方面,随着单台微波源功率的大幅提高和功率合成技术的发展,天线远场区的大气击穿问题越来越突出。如何判别是否存在大气击穿,如何确定判断的依据,都是需要解决的问题。论文提出依据击穿阈值和天线辐射场与高度关系曲线的变化规律进行判断。当HPM初始辐射场小于该区域大气击穿阈值,且上述两条曲线之间存在交点,即说明存在HPM辐射天线未击穿而传输路径近场区或远场区可能满足大气击穿条件的情况,这一现象也在相关实验中得到了证实。     

单极性亚纳秒脉冲激励口径的辐射特性

 通过解析积分运算，获得了阶跃脉冲激励口径天线瞬态辐射场的解析表达式, 分析了辐射电场脉冲的持续时间与口径尺寸、观察距离及观察角度的关系。研究了在高斯脉冲激励下口径辐射场特性的分析方法，并探讨了脉冲口径天线主轴方向上辐射场的分区依据。     

聚焦条件下的高斯波束矩形口径天线近场分析

 采用口径场法对聚焦条件下具有高斯波束的矩形口径天线近场进行了分析,得到了聚焦条件下的近场场强分布与近场增益解析式,并对不同的聚焦位置进行了仿真。结果表明：在近场区,聚焦位置离轴向越近,其场强越强,且增益越大,聚焦位置沿轴向时其场强与增益皆为最大;反之,聚焦位置离轴向越远,其近场场强与近场增益越小。因此,通过聚焦可以显著提高天线口径面场的近场场强与增益指标,从而提高天线系统的有效作用距离。     

高功率超宽带脉冲辐射实验装置研制

 研制了高功率超宽带脉冲辐射实验装置。该装置主要由脉冲充电电源、超宽带脉冲产生装置、超宽带脉冲发射天线三部分组成。达到的主要指标为：脉冲电源输出电压600 kV、重复频率100 Hz；脉冲压缩输出峰值功率约10 GW、脉宽1.2 ns；在辐射天线轴上220 m处，辐射峰值电场16.1 kV/m、等效辐射功率0.42×10¹² W；辐射场E面方向图半功率宽度为8°，H面方向图半功率宽度为9°。     

TEM喇叭馈源与共面馈源脉冲辐射天线性能比较

在反射面尺寸一定的情况下,优化设计了 TEM喇叭馈源与共面馈源脉冲辐射天线,并对比了两种天线的辐射性能。分析了反射面型脉冲辐射天线的工作机理,通过准静态近似,分别得到了两种天线的远区辐射场解析解。通过理论求解,得到了两种馈源在反射面口径造成的场分布,为天线结构设计提供参考。通过分析不同脉冲宽度时两种天线的辐射情况,比较了这两种馈源性能的优劣。完成了上述两种GW级高功率高效率馈源的研制,并开展了对比实验,实验结果与理论分析相吻合。     

大口径天线短脉冲微波辐射特性

为了开展大口径天线短脉冲微波辐射特性研究,建立了一套大口径天线微波短脉冲特性测试系统。该系统可产生快上升沿、脉冲可调(脉宽最短可到0.5 ns)的微波激励脉冲、接收动态范围大于52 dB。利用该测试系统进行实验,获得了不同微波激励脉冲宽度条件下,天线方向图和辐射场波形脉冲宽度变化曲线。测试结果表明:在天线远场距离处,改变微波激励脉冲宽度,对天线主轴辐射场波形基本无影响;而在偏离主轴处,辐射场波形会出现不同程度的脉冲展宽及幅值减小等波形畸变现象,偏离主轴角度越大,微波激励脉冲宽度越小,畸变越明显。     

高辐射效率超宽谱脉冲辐射天线的设计与实验

设计了一种采用共面TEM馈电结构的抛物反射面超宽谱脉冲辐射天线,分析了该种馈电结构的阻抗特性与辐射特性。实验表明当馈入电压为3kV、前沿180ps的超宽谱脉冲时,该天线主轴辐射场测试距离与峰值场强之积平均值达到18.3kV,相较于常用的TEM喇叭馈电的超宽带反射面天线,其辐射效率有了显著的提高。     

冲击脉冲辐射天线辐射场计算及应用

根据由张量法得到的任意线天线电场计算公式,利用镜像法推导,得到冲击脉冲辐射天线辐射电场的时域解析表达式。应用该表达式计算冲击脉冲辐射天线应用于辐射波电磁脉冲模拟器的时域辐射场,并与数值计算进行比较,结果表明:解析计算得到的辐射场波形与数值计算结果吻合较好,因此,利用解析表达式可以方便地观察天线结构参数对天线辐射场波形的影响,从而选取合适的参数以产生符合标准要求的天线场波形。     

TEM喇叭天线辐射机理分析和优化设计

在频域和时域研究了TEM喇叭天线的辐射机理。在频域,高频信号激励的TEM喇叭表现为口径天线的辐射特性,具有良好的方向性;低频信号激励的TEM喇叭可视作偶极子天线,具有全向辐射特性;在时域,脉冲激励的TEM喇叭天线辐射场由四个子波叠加构成,在不同方向上,各个子波的波形和相对时序不同,导致不同方向上辐射场波形也不相同。根据辐射机理研究结果,提出了一种TEM喇叭天线末端加载设计并给出了其优化设计方法,有效地改善了天线主轴辐射性能,提高了辐射因子和天线效率。     

TEM喇叭天线脉冲辐射特性

采用时域有限积分法（FIT）对相同几何口径尺寸下不同长度TEM喇叭天线的主轴辐射特性进行了研究,分析了有限长TEM喇叭天线与理想（无限长）TEM喇叭天线主轴辐射场存在差异的原因,导出了有限长TEM喇叭天线主轴辐射场在接近理想TEM喇叭天线辐射场条件下天线长度与激励脉冲宽度（或脉冲上升时间）之间的关系。在此基础上,根据文献中的研究结果,并结合激励脉冲波形,给出了TEM喇叭天线几何参数的优化设计方法。     

有限振幅声波间的非线性相互作用对声源远场指向性的影响

根据Fenlon理论推导得到了多频声源的辐射声压.基于单频声源谐波指向性的求解方法,得到了二阶近似下的双频声源辐射出的声波相互作用时的远场指向性.分别研究和讨论了在初始辐射声压和频率不同情况下,两列波的相互作用对其中一列波的一阶波和二阶波远场指向性的影响.结果表明,声波间的相互作用对声源远场指向性的影响根据各波之间的相对初始辐射声压和相对频率的不同而有所变化. 关键词： 有限振幅声波 非线性相互作用 远场指向性     

A numerical method for computation of sound radiation from an unflanged duct

Some issues involved in establishing a numerical model for sound radiation from a straight duct are addressed in this paper. The main ingredient of the numerical method is solutions of linearized Euler equations using a high order compact scheme. Farfield directivity is estimated through an integral solution of Ffowcs-Williams Hawkings equations. A generic test case of planar wave radiation from an unflanged duct is studied. The sound pressure level and wave propagation in the nearfield are analyzed, together with the farfield directivity. Comparison with analytical solutions shows good agreement. The effect of grid resolution on the sound radiation pattern and the construction of integration surface on the farfield directivity are discussed.     

球冠型换能器声辐射指向性分析

为了研究球冠型换能器的声辐射特性,在分离变量法求解球面坐标系下波动方程的基础上,采用基于球谐基傅里叶变换及边界条件的求解模型,给出了球冠型换能器声辐射的远场声压计算表达式和远场指向性表达式;仿真计算了球冠换能器的远场指向性随球冠极角、球半径及振动频率变化的特性,球冠所在球障板的直径和介质中声波的波长比决定着球冠声辐射指向性,在低频或波长大于球障板直径时,球冠声辐射呈无指向性,随着频率的增高即波长的减小或者球障板直径的增大,球冠声辐射的指向性越明显,波束开角越趋向于球冠的开角,而且波束开角内出现波浪状起伏越明显;试制了高频球冠型换能器基阵,测试了换能器基阵300 kHz的指向性,测试结果与理论计算相符合,验证了理论计算表达式的正确性,可为设计球冠型换能器及基阵提供理论指导。      

Three-dimensional analysis of scattering by pressure-release plane surfaces and the validity of the image solution

Because of the complexity of the scattering integrals in three dimensions, numerous approximations are used to obtain closed-form solutions. By considering the scattering by an infinite, pressure-release plane surface, the effects of various phase approximations and source directivity approximations can be examined independently of the surface roughness. Calculations are carried out using the Fraunhofer and Fresnel phase approximations, and two directivity approximations. It has been shown experimentally that the image solution is valid for the reflection of an acoustic beam by an infinite, pressure-release plane surface if the plane is in the farfield of the source. Consequently, the image solution is used to compare analytical solutions obtained using various phase and directivity approximations, and it is found that both the Fresnel phase approximation and a realistic directivity approximation are required to achieve a good fit. The solution produced by the Fraunhofer phase approximation is obtained as an asymptotic limit of the modified Fresnel solution. Criteria for the validity of the Fraunhofer and Fresnel phase approximations are developed. The Fresnel phase approximation is valid under fairly broad conditions, but the Fraunhofer phase approximation is never valid for an infinite plane surface that must be in the farfield of the source.     

渐进多焦点镜片波前像差的扩束测量方法

利用波前传感器测量自由曲面镜片时,由于自由曲面镜片的直径通常大于波前传感器的接收孔径,主要采用子孔径拼接技术测量镜片的波前像差。针对子孔径拼接技术测量中存在着操作繁琐、数据处理量大等问题,提出渐进多焦点镜片波前像差的扩束测量方法,得到渐进多焦点镜片中央直径为22 mm圆形区域内的波前像差。为了验证试验的可靠性,将测量得到的波前像差泽尼克表述中的离焦项转换为球镜度,与条纹偏折法测量得到镜片的球镜度进行对比实验,实验结果证明了渐进多焦点镜片波前像差的扩束测量方法可以用于渐进多焦点镜片波前像差的检测。     

Analysis of acoustic directivity of spherical cap transducers

In order to study the acoustic radiation from the spherical cap transducer,a theoretical model is used by solving the wave equation in spherical coordinates using the method of separation of variables,based on the spherical harmonic Fourier transform and boundary condition.The calculation formulas for the far field radiated pressure and directivity of spherical cap are derived.Some theoretical results are presented in the form of far-field directivity patterns of the spherical cap transducer for various polar angles of the spherical cap,radii of sphere baffle and operating frequencies.Both the diameter of the sphere baffle and the wavelength determine the directivity of acoustic radiation from a spherical cap.When the frequency is lower or the wavelength is longer than the diameter of the sphere baffle,the acoustic radiation from a spherical cap is omnidirectional.With the increase of the frequency or the diameter of the sphere baffle,the acoustic radiation from a spherical cap is more directional and the beamwidth more tends to spherical cap angle.Furthermore,the ripple in the beam is more obvious.The high frequency spherical cap transducer was fabricated and the directivity pattern was tested and the measurement data is shown to coincide with the theoretical results.This research can provide a guideline for designing the spherical cap transducers and arrays.     

Transient dipolar sound wave in a viscous compressible fluid

The dipolar sound wave generated by a sudden impulse in an unbounded viscous compressible fluid is studied on the basis of the linearized Navier-Stokes equations. Due to viscosity the spherical wavefront is diffuse with a width which grows with the square root of time. The wavefront is followed by a spherical shell of static potential flow. The shell itself surrounds an expanding spherical region of viscous flow. At long times the energy in each of the three regions is of comparable magnitude, and decays with a t^−3/2 power law.     

Radiation field of spherical mirror antennas

The unique features of radiation pattern formation in spherical mirror antennas are determined. It is shown that in antennas of this type there is a possibility of doubling directivity by placement of the feed at the paraxial focus. Equations are developed for calculation of the optimum feed placement, effective aperture radius, directional pattern width, and side lobe level. It is shown that side-lobe radiation from a spherical mirror antenna is formed by geometric optical reflection of the feed field on the peripheral portion of the mirror.Sevastopol Instrument Engineering Institute. Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Radiofizika, Vol. 34, No. 2, pp. 173–176, February, 1991.     

HIGH-WAVENUMBER ACOUSTIC RADIATION FROM A THIN-WALLED AXISYMMETRIC CYLINDER

The radiation from an axisymmetric thin-walled cylinder is determined by using the Geometrical Theory of Diffraction. The non-uniformities associated with this theory are corrected by using uniform asymptotic techniques, and the farfield velocity potential is calculated everywhere. The theory provides a paradigm for interpretation of geometrical features of the directivity pattern in the far field, and the results are discussed from this perspective. Comparison is made with analytical results obtained by using the Wiener-Hopf technique and the agreement is shown to be excellent. In particular, the uniform asymptotic techniques give the correct farfield form of the velocity potential in the principal lobe and predict the value at the peak of the principal lobe very accurately. This work provides a theoretical basis for the investigation of the radiation from asymmetric cylinder apertures, which has important applications in the noise reduction of aircraft, and which is discussed in a companion paper.     

Source characterization of a subsonic jet by using near-field acoustical holography

In the present study, patch near-field acoustical holography was used in conjunction with a multireference, cross-spectral sound pressure measurement to visualize the sound field emitted by a subsonic jet and to predict its farfield radiation pattern. A strategy for microphone array design is described that accounts for the low spatial coherence of aeroacoustic sources and for microphone self-noise resulting from entrained flow near the jet. In the experiments, a 0.8-cm-diameter burner was used to produce a subsonic, turbulent jet with a Mach number of 0.26. Six fixed, linear arrays holding eight reference microphones apiece were disposed circumferentially around the jet, and a circular array holding sixteen, equally spaced field microphones was traversed along the jet axis to measure the sound field on a 30-cm-diameter cylindrical surface enclosing the jet. The results revealed that the jet could be modeled as a combination of eleven uncorrelated dipole-, quadrupole-, and octupole-like sources, and the contribution of each source type to the total radiated sound power could be identified. Both the total sound field reconstructed in a three-dimensional space and the farfield radiation directivity obtained by using the latter model were successfully validated by comparisons to directly measured results.