小型射流发生器的实验研究

通过对小型射流单重态氧发生器的稳定工作条件及射流板性能对发生器的性能影响的考察,在一个小型超音速氧碘化学激光器中使用射流发生器成功地得到激光输出.     

小型射流发生器的实验研究

通过对小型射流单重态氧发生器的稳定工作条件及射流板性能对发生器的性能影响的考察,在一个小型超音速氧碘化学激光器（COIL）中使用射流发生器成功地得到激光输出。     

射流式氧发生器的三维模拟研究

实现了对射流式氧发生器的三维仿真模拟,给出了氧发生器内部流场结构、各组分的分布状态等信息。研究了射流孔结构对氧发生器性能的影响。指出即便是具有相同比表面积的不同射流孔排布方式,也会对发生器性能产生影响。此外,逆向射流式氧发生器反应器中气体从双侧进入对于减小发生器对气体的阻力具有重要作用。     

激光器件 化学激光器

TN248．5 2005031734 横向射流式单重态氧发生器的性能实验研究=Experi- mental investigation on performance of transverse jet sin- glet oxygen generator[刊,中]／张岳龙(中科院大连化物 所．辽宁,大连(116023)),房本杰…∥强激光与粒子束,- 2004,16(8).-997-999 对氧碘化学激光器的单重态氧发生器(SOG)进行了 改进,采用横向射流方式,并对该横向射流式单重态氧发 生器的性能进行了检测。实验中过氧化氢碱溶液温度控 制在-16℃左右,氯气流量为530 mmol／s,He与氯气的 流量比为3。采用PS法测量单重态氧分子的产率,吸收法     

COIL中稀释气体对单态氧产率影响的实验研究

 利用自发Raman散射光谱对射流式氧发生器的单态氧产率进行了测试，研究了稀释气体对于发生器产率的影响，并分析了造成影响的原因     

横向射流式单重态氧发生器的性能实验研究

 对氧碘化学激光器的单重态氧发生器（SOG）进行了改进，采用横向射流方式，并对该横向射流式单重态氧发生器的性能进行了检测。实验中过氧化氢碱溶液温度控制在－16℃左右,氯气流量为530mmol/s，He与氯气的流量比为3;采用PS法测量单重态氧分子的产率,吸收法测量氯气的利用率和相对水含量。得出如下结论:在不使用冷阱和分离器的情况下，最高单重态氧分子产率达到58%, 氯气利用率在80%以上,相对水含量小于等于0.5;气体达到最大流量时,发生器仍然能稳定地工作。     

射流式单重态氧发生器理论模型

 射流式单重态氧发生器(JSOG)是化学氧碘激光器十分重要的能源部分，它主要是通过解气相、液相扩散方程来求解发生器出口的氯的利用率和单重态氧的产率。在实际工作中的射流发生器非常复杂，其扩散方程和边界条件为非线性，非齐次边界条件，非齐次泛定方程组，求解难度较大。通过边界条件，采用试探解的方法，解得氯、总氧、单重态氧的气相、液相扩散方程，得到了氯的利用率，及单重态氧产率的解析解，与实验结果基本相符。     

单重态氧发生器出口气流中O2(1△)及水汽绝对浓度的测量

单重态氧发生器是氧碘化学激光器的核心部件．O2(^1△)和水汽的粒子数密度(绝对浓度)是单重态氧发生器的两个重要参量，其中O2(^1△)是氧碘化学激光器的能源，而水汽对氧碘化学激光器的发光介质-I^ 有强烈的淬灭作用。如何简单准确地测量这两个参量，一直是氧碘化学激光器研究中的一个难题。利用体光源模拟标定法，得到了O2(^1△)和水汽的绝对浓度，并且成功地用一套实验装置对射流式单重态氧发生器的上述两个参量进行了实时测量，得到了两个参量的变化曲线，同时还提供了O2(^1△)的产率以及水汽体积浓度等参量的变化曲线，通过大量实验结果，给出了各参量的变化规律，为射流式单重态氧发生器研究提供了有力的参考依据。     

单重态氧发生器出口气流中O_2(~1Δ)及水汽绝对浓度的测量

单重态氧发生器是氧碘化学激光器的核心部件 ,O2 (1Δ)和水汽的粒子数密度 (绝对浓度 )是单重态氧发生器的两个重要参量 ,其中O2 (1Δ)是氧碘化学激光器的能源 ,而水汽对氧碘化学激光器的发光介质—I 有强烈的淬灭作用。如何简单准确地测量这两个参量 ,一直是氧碘化学激光器研究中的一个难题。利用体光源模拟标定法 ,得到了O2 (1Δ)和水汽的绝对浓度 ,并且成功地用一套实验装置对射流式单重态氧发生器的上述两个参量进行了实时测量 ,得到了两个参量的变化曲线 ,同时还提供了O2 (1Δ)的产率以及水汽体积浓度等参量的变化曲线 ,通过大量实验结果 ,给出了各参量的变化规律 ,为射流式单重态氧发生器研究提供了有力的参考依据。     

SDBD等离子体增强双股矩形射流掺混性能实验研究

为提高姿轨控液体火箭发动机同轴式喷注器掺混性能,设计了简化的双股矩形射流发生器,开展了等离子体控制射流实验,获得了射流流场结构与速度分布,结果表明与单股射流类似,双股矩形射流同样具有很好的相似性,随着射流速度差的增大,相似性进一步增强,混合点逐渐靠近射流发生器出口,混合角和混合率增大,而涡量最大值减小;等离子体对射流相似性的影响较弱,主要增大了发生器出口附近的速度,缩短了射流核心区长度,增大了射流宽度和混合角,使得混合点位置移向发生器出口,扩大了高涡量值区域范围,不过3种实验工况下射流涡量和的正、负值均比较接近,混合率也非常接近,并且随着射流速度差的增大,等离子体控制效果降低;总的来说,等离子体激励器应安装在低速射流中,增大混合角比控制混合点位置对提高混合率更有效.      

JSOG中水蒸汽含量的模拟计算

 氧碘化学激光（简称 COIL）系统中，水是影响激光功率输出的最重要的原因之一。气流中的水不仅对激发态碘原子有严重的猝灭作用，另外对碘分子解离、超音速流动特性也有很坏的负面作用。单重态氧发生器的BHP（Basic Hydrogen Peroxide ）溶液是最主要的水蒸汽源。利用传质模型对射流式单重态氧发生器（简称JSOG）中产生的水蒸汽进行了计算，所得的数值结果与实验测量结果基本相符。根据模拟结果，对发生器的设计及实验条件进行了优化。     

Characterization and Studies on Hydro Dynamically Stable Operation of an Angular Jet SOG for COIL

Chemical oxygen-iodine Laser (COIL) is one of the fast emerging high power laser source for near Infrared (=1.315m) laser generation. The heart of the system is the singlet oxygen generator (SOG) which is a pumping source for this laser. A Jet type SOG with a novel approach was designed and fabricated. Singlet oxygen was taken out of the SOG at an angle of 40° thus avoiding the carry over of droplets, which is one of the major drawbacks of horizontal system. The preliminary results have been reported in our earlier publication. The present paper discusses the performance of this generator for various operational conditions viz. diluent's gas nitrogen / helium, basic hydrogen peroxide composition, generator pressure and gas velocity. Further, conditions for the stable operation from generator as well as chlorine injection point of view have been identified.     

On the flow behaviour of combustion gas in the boundary layer of MHD generators

The flow behaviour of combustion gas in the boundary layer of a small-scale MHD generator has been reviewed in the light of empirical conclusions drawn by Onda, Kaga, and Kato.     

自发喇曼成像法在线测量流场组分浓度

 介绍了自发喇曼成像技术实时监测流场组分浓度的方法,利用Nd：YAG脉冲激光器以及ICCD和光谱仪对大气进行了不同实验条件的测试,得到了影响谱线强度及测试精度的几个因素;得到了大气流场各主要成分的自发喇曼散射光谱和绝对浓度,测量误差小于8%。该技术可望在氧碘化学激光器单重态氧发生器物种浓度测定时得以应用以改善O₂(¹Δ)浓度测试精度较低的现状。     

小尺度涡流发生器强化传热机理的研究

在矩形槽道内布置了不同高度的小尺度涡流发生器,采用湍流模型对流体在其中的流动与传热特性进行了数值模拟,并对流体在槽道中的传热和流动特性进行了对比研究.分析了小尺度涡流发生器诱导涡的特性及其对湍流相干结构的影响与作用,讨论了湍流相干结构对温度场的作用机理,解释了涡流发生器强化换热的机理.     

利用喇曼光谱测量氧碘激光器氧发生器的O2（a^1△）产率

利用自发喇曼成像技术实时监测氧碘激光器O2（a^1△）发生器流场组分，得到了发生器气流中O2（a^1△）和O2（X^3∑）以及N2的自发喇曼散射光谱，由此得到了不同条件下的O2（a^1△）产率。测量误差不超过8%。     

High throughput jet singlet oxygen generator for multi kilowatt SCOIL

A jet flow singlet oxygen generator (JSOG) capable of handling chlorine flows of nearly 1.5 mol s⁻¹ has been designed, developed, and tested. The generator is designed in a modular configuration taking into consideration the practical aspects of handling high throughput flows without catastrophic BHP carry over. While for such high flow rates a cross-flow configuration has been reported, the generator utilized in the present study is a counter flow configuration. A near vertical extraction of singlet oxygen is effected at the generator exit, followed by a 90° rotation of the flow forming a novel verti-horizontal COIL scheme. This allows the COIL to be operated with a vertical extraction SOG followed by the horizontal arrangement of subsequent COIL systems such as supersonic nozzle, cavity, supersonic diffuser, etc. This enables a more uniform weight distribution from point of view of mobile and other platform mounted systems, which is highly relevant for large scale systems. The present study discusses the design aspects of the jet singlet oxygen generator along with its test results for various operating ranges. Typically, for the intended design flow rates, the chlorine utilization and singlet oxygen yield have been observed to be ∼94% and ∼64%, respectively.     

Experimental and modeling study on the pyrolysis and oxidation of iso-octane

High pressure iso-octane shock tube experiments were conducted to assist in the development of a Jet A surrogate kinetic model. Jet A is a kerosene based jet fuel composed of hundreds of hydrocarbons consisting of paraffins, olefins, aromatics and naphthenes. In the formulation of the surrogate mixture, iso-octane represents the branched paraffin class of hydrocarbons present in aviation fuels like Jet A. The experimental work on iso-octane was performed in a heated high pressure single pulse shock tube. The mole fractions of the stable species were determined using gas chromatography and mass spectroscopy. Experimental data on iso-octane oxidation and pyrolysis were obtained for temperatures from 835 to 1757 K, pressures from 21 to 65 atm, reactions times from 1.11 to 3.66 ms, and equivalence ratios from 0.52 to 1.68, and ∞. Iso-octane oxidation showed that the fuel decays through thermally driven oxygen free decomposition at conditions studied. This observation prompted an experimental and modeling study of iso-octane pyrolysis using an iso-octane sub-model taken from a recently published n-decane/iso-octane/toluene surrogate model. The revised iso-octane sub-model showed improvements in predicting intermediate species profiles from pyrolytic experiments and oxidation experiments. The modifications to the iso-octane sub-model also contributed to better agreement in predicting the formation of carbon monoxide and carbon dioxide when compared to the recently published 1st Generation Surrogate model and a recently published iso-octane oxidation model. Model improvements were also seen in predicting species profiles from flow reactor oxidation experiments and ignition delay times at temperatures above 1000 K at both 10 and 50 atm.     

Studying the effect of flap angle on the noise of interaction of a high-bypass jet with a swept wing in a co-flow

Jet–flap interaction noise for a small-scale swept wing model of a trendsetter plane has been studied experimentally, with a double-stream nozzle installed nearby. The effect of the flap angle on the noise of jet–wing interaction has been analyzed. It has been discovered that the flap angle considerably affects the interaction noise in a wide frequency range in such a way that the noise intensity in each frequency band grows exponentially as the flap edge approaches the shear-layer boundary (on a logarithmic scale, this corresponds to linear scaling of the spectrum depending on the flap angle). The exponential noise reduction as the flap angle decreases agrees with the known theoretical simplified-configuration models that are based on the effect of interaction of the near field of instability wave with the edge. Not only does this agreement show that noise increase/reduction mechanism may be associated with similar processes, it also provides an effective tool for controlling the interaction noise.