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Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)最新文献

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Linear independent increment process with linear standard deviation function for degradation analysis 具有线性标准差函数的线性独立增量过程用于退化分析
Zhihua Wang, H. Fu, Yongbo Zhang
Degradation test is a feasible means to assess the failure time distributions of complex systems and highly reliable products. Generally speaking, the degradation process is essentially a continuous state random process. Motivated by the independent increment process theory, we propose a degradation analysis model, in which degradation is represented by an independent increment process with linear mean and standard deviation functions (quadratic variance function). A one-stage method is further developed to estimate the model parameters and failure time distribution. The methodology has been implemented in the analysis of GaAs laser degradation. The comparative results illustrate that the proposed method can be considered good and show a promise for future applications.
退化试验是评估复杂系统和高可靠性产品失效时间分布的一种可行手段。一般来说,退化过程本质上是一个连续状态随机过程。在独立增量过程理论的启发下,提出了一种退化分析模型,该模型将退化描述为具有线性均值和标准差函数(二次方差函数)的独立增量过程。进一步提出了一种单阶段估计模型参数和失效时间分布的方法。该方法已应用于砷化镓激光退化分析中。对比结果表明,该方法具有较好的应用前景。
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引用次数: 1
Design and development of a high power 1×5 splitter/combiner for solid state radar transmitters 用于固体雷达发射机的高功率1×5分路/合并器的设计与开发
M. S. Anwar, N. Ahsan, M. Shan
This paper presents an L-band non binary six port (1×5) power splitter/combiner utilizing stripline architecture. The detailed design, its implementation and testing is the main focus of this paper. The circuit optimization has been carried out utilizing ADS®. The paper also provides the comparison of simulation and measured results. The measured results indicate that the splitter/combiner has an amplitude balance of ± 0.8 dB with a frequency BW of 500MHz in L-band. Both Input and output VSWR is less than 1.55 while the worst case insertion loss is 0.36 dB. All these results make this combiner/splitter very useful for solid state amplifiers for radar applications.
本文提出了一种利用带状线结构的l波段非二进制六端口功率分配器/合成器(1×5)。详细设计、实现和测试是本文的重点。利用ADS®对电路进行了优化。文中还对仿真结果和实测结果进行了比较。测量结果表明,分配器/合成器在l波段的幅值平衡为±0.8 dB,频率BW为500MHz。输入输出驻波比均小于1.55,最坏情况下插入损耗为0.36 dB。所有这些结果使得该合并/分频器非常适用于雷达应用的固态放大器。
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引用次数: 0
Ethylene-propylene-diene terpolymer vulcanizates' reinforcement with precipitated silica 用沉淀二氧化硅增强乙烯-丙-二烯三元共聚物的硫化
I. Yousafa, S. Alib, S. Mirzac
Physical properties of rubber composites can be enhanced by employing the particulate fillers for example calcium carbonate, silica and carbon black. Modulus, tear & abrasion resistance usually have a tendency to increase by the incorporation of the fillers in elastomers. Particulate fillers like high-structured silica and carbon black, generally, offered considerable reinforcing effects. The key purpose of this paper is to study the impact of filler (Vulkasil C, precipitated silica) dosages/loading on the mechanical properties of interest for instance hardness, elongation at break, tensile strength and bound rubber of EPDM based rubber vulcanizates.
通过采用颗粒填料如碳酸钙、二氧化硅和炭黑,可以增强橡胶复合材料的物理性能。模量,撕裂和耐磨性通常有增加的趋势,通过在弹性体中掺入填料。颗粒填料,如高结构二氧化硅和炭黑,通常提供了相当大的增强效果。本文的主要目的是研究填料(Vulkasil C,沉淀二氧化硅)用量/载荷对EPDM基橡胶硫化胶的力学性能的影响,例如硬度,断裂伸长率,拉伸强度和结合橡胶。
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引用次数: 3
Multiband sensing-time-adaptive joint detection cognitive radios framework for Gaussian channels 高斯信道多频带感知-时间自适应联合检测认知无线电框架
S. Z. Farooq, A. Ghafoor
This paper analyzes the multiband sensing-time-adaptive joint detection cognitive radios framework. The framework optimizes secondary throughput while minimizing the interference to a wideband multiband primary communications system. The ranges are determined under which the problem can be categorized as a complex optimization one under real Gaussian channel conditions. Simulated results compare the performance of MSJD framework with the earlier proposed multiband joint detection (MJD) framework for some typical primary signals received in real Gaussian and Circularly Symmetric Complex Gaussian channels.
分析了多波段感知-时间自适应联合探测认知无线电框架。该框架优化了辅助吞吐量,同时最大限度地减少了对宽带多频带主通信系统的干扰。在此范围内,该问题可归类为实际高斯信道条件下的复杂优化问题。仿真结果比较了MSJD框架和MJD框架在实高斯和圆对称复高斯信道中接收的典型主信号的性能。
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引用次数: 5
Preparation and characteristic research on composites of polyphenylene sulfide modified by nano-silicon dioxide 纳米二氧化硅改性聚苯硫醚复合材料的制备及性能研究
Xiaojun Wang, Xiujuan Lu, Bo Xu, Jiping Liu
Pure PPS was modified by nano-SiO2, and mixed with SBS, PPA auxiliaries and smoke suppression agent. The compound materials were tested on dispersion homogeneity of nano-SiO2, water absorption, mechanics function, TEM and thermal properties. It discovered that the nano-SiO2 was homogeneous in PPS and it could decrease the water absorption rate and the temperature coefficient of expansion and improve the mechanical and thermal properties, as well as the performance life. The composite materials really satisfy the strict index demands of electron packing materials.
采用纳米sio2对纯PPS进行改性,并与SBS、PPA助剂和消烟剂混合。对复合材料的分散均匀性、吸水性、力学性能、透射电镜和热性能进行了测试。研究发现,纳米sio2在聚苯乙烯中具有均匀性,可以降低聚苯乙烯的吸水率和膨胀温度系数,提高聚苯乙烯的力学性能和热性能,提高聚苯乙烯的使用寿命。该复合材料完全满足电子封装材料严格的指标要求。
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引用次数: 0
Design & full-wave EM simulation of Ku-band orthomode transducer (OMT) ku波段正交换能器(OMT)的设计与全波电磁仿真
M. Latif, A. U. Salfi, M. Shafique
The paper describes the design and full-wave EM simulation of Ku-band (10.7-14.5) GHz orthomode transducer (OMT). The OMT designed is class 2 (symmetric OMT) which has higher fractional bandwidth and cross-polarization isolation than the class 1 OMT. It is realized with Modified Bfifot junction where the tuning pins are replaced with well placed capacitive steps. Moreover septum is four times thicker than conventional class 2 OMT, making it realizable up to 1 THz frequency. Cross-polarization isolation ≥ 80 dB and return loss ≥ 20 dB are achieved in the entire band. Effect of manufacturing tolerances and assembly misalignment are incorporated d the full-wave EM simulation. All the simulation & optimization work is done in industry standard EM Simulation software.
本文介绍了ku波段(10.7-14.5)GHz正交换能器(OMT)的设计和全波电磁仿真。设计的OMT是2类(对称OMT),它比1类OMT具有更高的分数带宽和交叉极化隔离。它是通过改进的Bfifot结实现的,其中调谐引脚被放置良好的电容级取代。此外,隔膜比传统的2级OMT厚四倍,使其可实现高达1太赫兹的频率。整个频段的交叉极化隔离度≥80 dB,回波损耗≥20 dB。在全波仿真中考虑了制造公差和装配误差的影响。所有的仿真和优化工作都在工业标准的电磁仿真软件中完成。
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引用次数: 5
Numerical simulation of pressure oscillations and instabilities in a solid propellant subscale motor 固体推进剂亚尺度发动机压力振荡和不稳定性的数值模拟
M. Ozair, M. N. Qureshi
It has been broadly reported in the literature that the large segmented solid rocket motors (SRMs), such as Ariane 5 solid booster (P230) and Space Shuttle RSRM (Re-designed SRM), experience undesirable pressure oscillations that lead to thrust oscillations during combustion due to a complex coupling between the combustion and the internal aerodynamics of the combustion chamber. These fluctuations adversely affect the rocket motor performance, could damage the payload and eventually cause mission failure. To investigate these instabilities, experiments on full-size motors are very expensive, complicated and time consuming, and are therefore not really suited for research. In this paper, LP6 motor, the 1/15- scale axisymmetric model of the Ariane 5 booster, is used to study the pressure oscillations and the vortex-shedding induced pressure instabilities. Computational Fluid Dynamics (CFD) simulations were carried out on a quadrilateral mesh of the LP6 geometry at the time of 6.4 s after ignition when the pressure oscillations were found to be almost peaked. Pressure oscillation frequencies and amplitudes obtained from CFD simulations are found to be in good agreement with experimental results obtained at ONERA (French National Aerospace Research Centre). From CFD simulations, it was also found that the potential source of instabilities and pressure oscillations in LP6 motor having no inhibitor rings or restrictors is the surface vortex shedding mechanism which is a phenomenon that has also been observed in the experiments. On the basis of the present study and results, CFD simulations can also be carried out for different geometric configurations and flow conditions in other SRMs to investigate the instabilities and pressure oscillations occurring in their combustion chambers.
文献中广泛报道了大型分段固体火箭发动机(SRM),如阿丽亚娜5号固体助推器(P230)和航天飞机RSRM(重新设计的SRM),由于燃烧和燃烧室内部空气动力学之间的复杂耦合,在燃烧过程中经历了不良的压力振荡,导致推力振荡。这些波动对火箭发动机性能产生不利影响,可能损坏有效载荷并最终导致任务失败。为了研究这些不稳定性,在全尺寸电机上进行实验是非常昂贵、复杂和耗时的,因此并不真正适合研究。本文利用阿丽亚娜5型助推器1/15比例轴对称模型LP6电机,研究了该助推器的压力振荡和旋涡脱落引起的压力不稳定性。在点火后6.4 s的四边形网格上进行了计算流体动力学(CFD)模拟,发现压力振荡几乎达到峰值。通过CFD模拟得到的压力振荡频率和振幅与法国国家航空航天研究中心(ONERA)的实验结果非常吻合。通过CFD模拟还发现,在无阻环和节流器的情况下,LP6电机不稳定和压力振荡的潜在来源是表面涡脱落机制,这一现象在实验中也得到了观察。在本研究和结果的基础上,还可以对其他srm的不同几何构型和流动条件进行CFD模拟,以研究其燃烧室内发生的不稳定性和压力振荡。
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引用次数: 0
Experimental study and CMFD modeling of transport processes in flow of two Immiscible liquids 两种不混相液体流动输运过程的实验研究与CMFD建模
M. Arshad, I. R. Chughtai, M. H. Inayat, A. Haq
Rectangular shaped sieve plate column was installed for study of transport parameters through high speed photography and image analysis. Two Immiscible liquids consisting of the dispersed phase (water) and continuous phase (kerosene oil) were introduced in countercurrent operation. Experiments were performed for dispersed and continuous phase superficial velocities 0.16-0.44 cm/sec and 0.37-0.47 cm/sec respectively, pulsation frequency 0.95 -1.72 rev/sec and pulsation amplitude 1cm. Upon increasing the superficial velocity of dispersed phase, its void fraction increases up to its asymptotic value and droplet velocity increase while the droplet size decreases. Upon increasing the pulsation frequency, its void fraction increases while the droplet size and droplet velocity decreases. A Computational Multi Fluid Dynamics simulation has been carried out in order to verify the experimental results using the FLUENT. The CMFD calculations for void fraction have been compared with the experimental results which have shown a maximum deviation of 2-3%.
安装矩形筛板柱,通过高速摄影和图像分析研究输送参数。逆流操作中引入了分散相(水)和连续相(煤油)两种不混相液体。脉动频率为0.95 ~ 1.72 rev/sec,脉动幅值为1cm,分散相表面速度为0.16 ~ 0.44 cm/sec,连续相表面速度为0.37 ~ 0.47 cm/sec。随着分散相表面速度的增加,其空隙率逐渐增大,直至其渐近值,液滴速度增大,液滴尺寸减小。随着脉动频率的增加,其空隙率增加,液滴尺寸和液滴速度减小。为了验证实验结果,利用FLUENT进行了计算多流体动力学仿真。将CMFD计算结果与实验结果进行了比较,结果显示最大偏差为2-3%。
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引用次数: 0
Experimental investigation of filament-wound composite tubes for mechanical characterization by internal pressure testing 纤维缠绕复合材料管力学性能内压试验研究
T. Rasheed, S. Akbar, S. Mirza
This paper presents method for the characterization of composite tubes produced by filament winding technique. The aim of this study is to investigate the mechanical properties by tensile test and under internal pressure loads. For this purpose specimens produced with different orientation having the same reinforcement with two different matrix systems. Data produced experimentally by measuring the mechanical properties like longitudinal tensile and hoop tensile properties, strain in hoop direction and maximum hoop stresses during the hydraulic testing. In order to investigate these parameters, internal pressure tests are done on the filament-wound composite tubes having internal diameter 64.5± 0.5 mm and length 320± 2.0 mm according to ASTM D 1599-99 standard. The tubes for the testing are manufactured by wet filament winding methods of [± 60°] E-glass/Epoxy of various wall thicknesses. Hydraulic tests revealed that the tubes with winding orientation [± 60°]2[±90°]2 exhibits better burst performance compared with others orientations. In addition, factors affecting the behavior of the tubes like buckling, stress variation through wall thickness are discussed.
本文介绍了长丝缠绕复合材料管的表征方法。本研究的目的是通过拉伸试验和内压载荷来研究其力学性能。为此,用两种不同的基体体系制作具有不同取向、相同配筋的试样。通过测量水力测试期间的纵向拉伸和环向拉伸性能、环向应变和最大环向应力等力学性能的实验数据。根据ASTM D 1599-99标准,对内径64.5±0.5 mm、长度320±2.0 mm的丝绕复合材料管进行了内压试验。用于测试的管是用不同壁厚的[±60°]e -玻璃/环氧树脂湿长丝缠绕法制造的。水力试验结果表明,缠绕方向为[±60°]2[±90°]2的管具有较好的爆破性能。此外,还讨论了影响管的屈曲、应力随壁厚变化等因素。
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引用次数: 1
Colloidal preparation of copper selenide and indium selenide nanoparticles by single source precursors approach 单源前驱体法制备硒化铜和硒化铟纳米颗粒
S. N. Malik, H. Ahmed, M. Shahid, N. Haider, M. Malik, P. O’Brien
Mx(iPr2PSe2)y] complexes (M = In, Cu) were synthesized by metathesis reaction of metal with ligand salt [HNEt3][iPr2PSe2]. These complexes undergo thermolysis in HDA/TOP at 200-270 °C, to yield monophasic Cu2-xSe and In2Se3 nanoparticles. Cu2-xSe nanoparticles (grown at 250 °C) and In2Se3 nanoparticles (grown at 270 °C) had a mean diameter of 5.0 ± 1.2 nm and 13 ± 2.5 nm, respectively.
采用金属与配体盐[HNEt3][iPr2PSe2]的复分解反应合成了Mx(iPr2PSe2)y]配合物(M = In, Cu)。这些配合物在200-270°C的HDA/TOP中进行热裂解,得到单相Cu2-xSe和In2Se3纳米颗粒。在250℃下生长的Cu2-xSe纳米粒子和在270℃下生长的In2Se3纳米粒子的平均直径分别为5.0±1.2 nm和13±2.5 nm。
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引用次数: 3
期刊
Proceedings of 2013 10th International Bhurban Conference on Applied Sciences & Technology (IBCAST)
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