VISAR测速中的信号丢失及丢失条纹数的确定

论述了ＶＩＳＡＲ测速中信号频率与被测速度增量的关系和光电倍增管、数字示波器所能响应的最高速度增量。分析了信号丢失的原因,给出了丢失条纹数的确定方法。最后对ＶＩＳＡＲ应用中如何正确选择条纹常数提出了建议。     

激光干涉测速技术在爆轰实验中的应用

用四探头ＶＩＳＡＲ系统测量了铜管外表面在冲击波作用下的膨胀速度以及各种材料（Ｃ１１,Ａｌ,Ｆｅ,玻璃）平面飞片的自由表面速度。是的圆筒壁面径向膨胀速度大于１４００ｍ／ｓ,平面飞片自由面运动速度大于５５００ｍ／ｓ,各被测样品的速度－时间曲线反映了物体的连续运动过程。     

The compression LS estimate of regression coefficient in multivariate linear model

ＴＨＥＣＯＭＰＲＥＳＳＩＯＮＬＳＥＳＴＩＭＡＴＥＯＦＲＥＧＲＥＳＳＩＯＮＣＯＥＦＦＩＣＩＥＮＴＩＮＭＵＬＴＩＶＡＲＩＡＴＥＬＩＮＥＡＲＭＯＤＥＬＣｈｅｎＳｈｉ－ｊｉ（陈世基）（Ｄｅｐｔ．ｏｆＭａｔｈｅｍａｔｉｃｓ,ＦＵｊｉａｎＮｏｒｍａｌＵｎｉｖｅｒ...     

Relativistic absoluteness of time-space-moving mass

ＲＥＬＡＴＩＶＩＳＴＩＣＡＢＳＯＬＵＴＥＮＥＳＳＯＦＴＩＭＥ－ＳＰＡＣＥ－ＭＯＶＩＮＧＭＡＳＳＣｈｉｎＹｕａｎｓｈｕｎ（秦元勋）（ＩｎｓｔｉｔｕｔｅｏｆＡｐｐｌｉｅｄＭａｔｈｅｍａｔｉｃｓＡｃａｄｅｍｉａＳｉｎｉｃａＣｈｉｎａ,Ｂｅｉｊｉｎｇ１０００...     

THE MAXIMUM DISSIPATIVE EXTENSION OFSCHRODINGER OPERATOR

ＴＨＥＭＡＸＩＭＵＭＤＩＳＳＩＰＡＴＩＶＥＥＸＴＥＮＳＩＯＮＯＦＳＣＨＲＯＤＩＮＧＥＲＯＰＥＲＡＴＯＲＴｉａｎＬｉ－ｘｉｎ（田立新）（ＤｅｐａｒｔｍｅｎｔｏｆＭａｔｈｅｍａｔｉｃｓａｎｄＰｈｙｓｉｃｓ,ＪｉａｎｇｓｕＩｎｓｔｉｔｕｔｅｏｆＴｅｃｈｎｏ...     

A modified method of averaging for solving a class of nonlinear equations

ＡＭＯＤＩＦＩＥＤＭＥＴＨＯＤＯＦＡＶＥＲＡＧＩＮＧＦＯＲＳＯＬＶＩＮＧＡＣＬＡＳＳＯＦＮＯＮＬＩＮＥＡＲＥＱＵＡＴＩＯＮＳＺｈａｎｇＢａｏ－ｓｈａｎ（张宝善）（ＤｅｐａｒｉｍｅｎｔｏｆＭａｉｈ．,ＸｕｚｈｏｕＴｅａｃｈｅｒｓＣｏｌｌｅｇｅ,Ｘｕｚｈ...     

INITIAL BOUNDARY VALUE PROBLEMS FOR A CLASS OF NONLINEAR INTEGRO－PARTIAL DIFFERENTIAL EQUATIONS

ＩＮＩＴＩＡＬＢＯＵＮＤＡＲＹＶＡＬＵＥＰＲＯＢＬＥＭＳＦＯＲＡＣＬＡＳＳＯＦＮＯＮＬＩＮＥＡＲＩＮＴＥＧＲＯ－ＰＡＲＴＩＡＬＤＩＦＦＥＲＥＮＴＩＡＬＥＱＵＡＴＩＯＮＳＣｕｉＳｈａｎｇ－ｂｉｎ（崔尚斌）（Ｄｅｐｔ．ｏｆＭａｔｈ．,ＬａｎｚｈｏｕＵｎｉ...     

Dissipative effects of an isolated bubble in water on the sound wave

ＤＩＳＳＩＰＡＴＩＶＥＥＦＦＥＣＴＳＯＦＡＮＩＳＯＬＡＴＥＤＢＵＢＢＬＥＩＮＷＡＴＥＲＯＮＴＨＥＳＯＵＮＤＷＡＶＥＨｕｎａｇＪｉｎｇ－ｑｕａｎ（黄景泉）ＬｉＦｕ－ｘｉｎ（李福新）（ＮｏｒｔｈｗｅｓｔｅｒｎＰｏｌｙｔｅｃｈｎｉｃＵｎｉｖｅｒｓｉｔｙ,Ｘ...     

A uniformly valid asymptotic solution of the Navier-Stokes equations

ＡＵＮＩＦＯＲＭＬＹＶＡＬＩＤＡＳＹＭＰＴＯＴＩＣＳＯＬＵＴＩＯＮＯＦＴＨＥＮＡＶＩＥＲ－ＳＴＯＫＥＳＥＱＵＡＴＩＯＮＳＱｉｎＳｈｅｎｇ－ｌｉ（秦圣立）ＺｈａｎｇＡｉ－ｓｈｕ（张爱淑）（Ｄｅｐｔ．ＯｆＰｈｙｓｉｃｓ,ＱｕｆｕＴｅａｃｈｅｒｓＵｎｉｖｅ...     

Iterative process for lipschitz local strictly pseudocontractive mappings

ＩＴＥＲＡＴＩＶＥＰＲＯＣＥＳＳＦＯＲＬＩＰＳＣＨＩＴＺＬＯＣＡＬＳＴＲＩＣＴＬＹＰＳＥＵＤＯＣＯＮＴＲＡＣＴＩＶＥＭＡＰＰＩＮＧＳＤｅｎｇＬｅｉ（邓磊）（ＣｈｏｎｇｑｉｎｇＴｅａｃｈｅｒ＇ｓＣｏｌｌｅｇｅ,Ｙｏｎｇｃｈｕａｎ,Ｃｈｏｎｇｑｉｎｇ）Ｄ...     

爆炸箔起爆器小尺寸飞片速度测试

设计了一套爆炸箔起爆装置,通过精确控制桥箔-飞片-加速腔三者的定位,在飞片表面镀一定厚度的铝膜（铝膜的质量与飞片的质量相比可忽略）,合理选择VISAR探头的工作距离和与干涉腔延迟时间相关的条纹常数,屏蔽测试系统以及加设滤光片等,利用VISAR测试技术有效解决了小尺寸飞片速度的测试问题。给出了两种尺寸0.7 mm0.025 mm和0.5 mm0.025 mm飞片的速度测试结果。结果表明,采取新的措施后,获得了信噪比好、能正确反映爆炸箔起爆器驱动飞片物理过程的信号和飞片速度历史。     

VISAR数据处理新方法及程序

分析了不同VISAR数据处理方法的原理 ,并在此基础上开发了新的VISAR数据处理程序。该程序采用极坐标法作为计算内核 ,消除了各路信号的不灵敏区 ;计算所需的各个参数相位差、振幅因子的比值 等采用参数拟合的方法从实验信号本身得出 ;程序可以处理信号缺失的情况 ,当四路信号只取得三路时 ,数据处理能照样进行 ;程序的后期处理功能可以判断丢失条纹的数目并恢复速度历史。初步讨论了参数误差对结果的影响。     

高灵敏度VISAR研究与设计

针对VISAR测速系统中的速度灵敏度问题 ,提出了折返式标准具设计 ,有效地提高了现有仪器的速度灵敏度 ,并就此设计进行了动态实验 ,实际测试了炸药驱动钢飞片自由面速度历史 ,取得了较好的测试结果。     

The development and application of a fast-response DC-coupled flame ionization current sensor

The principles of the design of a fast-response DC-coupled ionisation probe and associated electronic circuit are described for the measurement of the mean and fluctuating components of the ion concentration in the reaction zones of stationary and transient flames. The performance of the ionisation probe is evaluated by bench tests and with measurements of ion current mean and fluctuating levels in laminar and turbulent premixed flames and in the combustion chamber of a spark ignition engine. The results demonstrate the wide frequency bandwidth, good spatial resolution and electronic noise immunity of the ionisation probe, making it suitable for a host of combustion applications.     

Analysis of intermittency and probe data in a supersonic flow with injection

 Probe measurements were performed in the flow field produced by injection of helium or air into a supersonic airstream. The injectant was seeded with water and Rayleigh scattering was used to image the injectant plume. The region of the flow containing injectant–air mixture is seen to be highly unsteady, leading to the intermittent presence of injectant in certain regions. The intermittency is inferred. It is shown that bias errors can occur when the probe data is analyzed by techniques which assume steady flow. A technique for relatively bias-free analysis utilizing the intermittency measurements is presented and the bias errors are estimated. The gas-sampling probe is shown to measure the mass-weighted-mean mass fraction of helium, which is significantly less than the simple mean. A new measure of mixing efficiency obtained from the combined probe and intermittency measurements is discussed. Received: 2 February 1996/Accepted: 2 December 1996     

An experimental study on the efficiency of transpiration cooling in laminar and turbulent hypersonic flows

An experimental study on the efficiency of transpiration cooling in hypersonic laminar and turbulent flow regimes is carried out in the Hypersonic Windtunnel Cologne with a focus on the aerothermal problems downstream of the cooled model part. The model is made of a material of low thermal conductivity (PEEK) with an integrated probe of a porous material. The experimental setup allows the direct comparison of the thermal behavior of transpiration cooling to a well-defined and radiatively cooled reference surface. Experiments are performed at Mach number of 6 and two different Reynolds numbers. Air, argon and helium are used as coolants at various flow rates, in order to identify the influence of coolant medium on cooling efficiency. The cooling efficiency of air and argon is comparable. Helium provides significantly higher cooling efficiency at the same blowing ratio, i.e. same coolant mass flow rate. The experimental data shows that the efficiency of the transpiration cooling in turbulent flows is much lower than in laminar flow.     

Benchmarking and improvements of measurement techniques for local-time-averaged two-phase flow parameters

Accurate measurements of local time-averaged two-phase flow parameters is of fundamental importance for the evaluation of two-phase flow models as well as for the development of closure relations used in the two-fluid model. For cross-calibration purposes, we compared the measurements of local-time-averaged two-phase flow parameters using a four-sensor conductivity probe developed by the TRSL (Thermal-hydraulics and Reactor Safety Laboratory) at Purdue University, and a four-sensor optical probe developed by the CEA (French Atomic Energy Commission). A system coupling methodology was also performed in order to isolate the effects of each instrumentation's components, i.e., probe, acquisition, thresholding, and processing effects. Experimental results have shown a reasonable agreement in the local void fraction, local bubble velocity, and local interfacial area concentration measurements comparisons. However, it is shown that particular attention must be given to the sensor probe design in order to get accurate measurements.     

激光速度干涉仪测量法在炸药圆筒试验中的应用

在炸药标准圆筒试验中 ,除了使用电探针测量炸药爆速、用高速相机记录圆筒膨胀过程的传统试验方法外 ,还用激光速度干涉仪 (VISAR)直接测量圆筒表面速度。根据圆筒试验的二维爆轰数值模拟分析结果 ,分析比较了高速相机和激光速度干涉仪的测量结果。     

激光干涉测速中信号光纤的模式色散对速度测量的影响

详细分析了测量任意反射面的激光干涉测速系统(VISAR)中信号光纤的模式色散对速度测量的影响,建立了数学分析模型,数值模拟了色散对比度因子与测速系统所使用的条纹常数和被测速度增量之间的关系。研究结果表明:（1）测速时使用的条纹常数越大,信号光纤模式色散的影响越小;（2）被测速度越大,信号光纤模式色散的影响越大;（3）阶跃折射率光纤的色散影响比剃度折射率光纤大得多。通过本项研究,给出了减小信号光纤模式色散的有效措施,对提高VISAR的干涉图对比度及测试精确度具有重要作用。     

Benchmarking of the five-sensor probe method for a measurement of an interfacial area concentration

Interfacial area concentration (IAC) is one of the most important parameters in the two-phase flow models. Five-sensor probe method is a useful measurement technique to measure an IAC. It is essentially based on the four-sensor probe method but it is improved by adapting one more sensor. The passing types of the interfaces through the sensors are classified into four categories and independent methods are applied to the interfaces belonging to each category. To verify the applicability of the five-sensor probe method, benchmarking tests are performed for a rectangular visual channel by using the photographic method. The bubble velocity, void fraction, and Sauter mean diameter measured by the probe are also benchmarked. This paper also includes the design of the five-sensor conductivity probe, the IAC measurement method, the signal processing procedure of the probe signal and the data analysis method by photography.