基于法布里-珀罗调谐滤波器的傅里叶域锁模扫频激光光源

报道了一个光纤型1300 nm波段的傅里叶域锁模(Fourier domain mode locking, FDML)扫频激光光源, 用于扫频光学相干层析成像技术 (optical coherence tomography, OCT) 成像. 本实验扫频激光光源采用包含增益介质、调谐滤波器和延迟线组成的长腔激光谐振腔以及光功率增强单元. FDML扫频激光光源具有快速和高度稳定运转模式, 相位稳定性好. 基于法布里-珀罗调谐滤波器(fiber Fabry-Perot tunable filter, FFP-TF)的FDML扫频激光光源扫频范围为130 nm, 半高全宽为70 nm, 输出平均功率是11 mW. 与基于FFP-TF的短腔的扫频光源做了对比研究, FDML扫频光源速度从短腔的8 kHz提高到了48.12 kHz, 对应生物组织OCT成像轴向分辨率为7.8 μm, 比短腔的减小了1.9 μm. 关键词： 光学相干层析技术 扫频激光光源 傅里叶域锁模 法布里-珀罗调谐滤波器     

考虑熵层效应的扫掠激波/湍流边界层干扰特性研究

为了探究熵层对扫掠激波/湍流边界层干扰特性的影响规律,采用仿真方法对尖鳍/钝板物理模型进行研究。结果表明：扫掠激波上游的熵层厚度随着平板前缘钝化半径的增大而增加,同时边界层厚度也随着熵层厚度的增加而增加。熵层的引入并不改变扫掠激波/湍流边界层干扰固有的准锥形相似特性,也不会改变拟锥原点(virtual conical origin, VCO)的位置,仅会改变干扰形成的上游影响线和分离线的角度。扫掠激波/湍流边界层干扰形成的锥形主旋涡和角涡的尺度随着熵层厚度的增加而增大。上游熵层的引入增大了下游扫掠激波/湍流边界层干扰区的总压损失,但扫掠激波/湍流边界层干扰自身造成的相对总压损失并不受上游熵层的影响。     

Polarization-maintaining buffered Fourier domain mode-locked swept source for optical coherence tomography

A polarization-maintaining buffered Fourier domain mode-locked (FDML) swept source with a center wavelength of 1300 nm is demonstrated. The scanning rate of the buffered FDML swept source is doubled without sacrificing the output power of the swept source by combining two orthogonally polarized outputs with a polarization beam combiner. The stability of the swept source is improved because the polarization state of the laser beam inside the laser cavity is maintained without the use of any polarization controllers. The swept source is capable of an edge-to-edge tuning range of more than 150 nm and a FWHM range of 95 nm at a 102 kHz sweeping rate and with an average power of 12 mW. A swept source optical coherence tomography (SSOCT) system is developed utilizing this buffered FDML swept source. The axial resolution of the SSOCT system is measured to be 9.4 μm in air. The sensitivity of the SSOCT system is 107.5 dB at a depth of 0.25 mm with a 6 dB roll-off at a depth of 2.25 mm.     

叶片尾缘掠型对离心压气机特性影响研究

针对叶片尾缘掠型对离心压气机特性影响开展了数值仿真与试验验证的研究工作,详细分析了尾缘掠型对压气机特性的影响规律和压气机叶轮内部流动特征,研究结果表明:尾缘掠型能够提升压气机出口的总压,使离心压气机压比变高,自由掠叶型相比于斜掠叶型,压比会进一步提升.叶片尾缘掠型能够有效抑制尾缘流动分离与叶间泄漏效应的结合效果,降低流...     

Duration discrimination of steady and gliding tones: a new method for estimating sensitivity to rate of change

Thresholds for the detection of differences in duration were measured in a two-alternative, forced-choice task for four types of signals, all centered at 2000 Hz: (1) sinusoids fixed in frequency and level; (2) sinusoids of fixed frequency whose level was swept up or down by 5 or 10 dB; (3) sinusoids of fixed level whose frequency was swept up or down by 100 Hz; and (4) sinusoids whose level was swept up or down by 10 dB and whose frequency was swept up or down by 100 Hz. For types (2)-(4), the direction of the sweeps was fixed within a run. The duration of the standard was either fixed at 750 ms or was varied randomly from trial to trial by up to +/- 7% about 750 ms. The duration of the comparison signal was initially 100 ms greater than that of the standard and was varied adaptively to determine threshold. The pattern of results was similar for all four subjects tested. Duration-discrimination thresholds for the signals that were swept in level and/or frequency were lower than those for the fixed signal, typically by 15-20 ms. This indicates that subjects were sensitive to the rate of change of frequency and/or level and could use this as a cue for duration discrimination. The Weber fraction for rate of change was estimated to be about 0.05-0.06 and was similar for changes in level and in frequency.     

Broadband and high-speed swept external-cavity laser using a quantum-dot superluminescent diode as gain device

A wide wavelength tuning range swept external-cavity laser using an In As/Ga As quantum-dot superluminescent diode as a gain device is demonstrated. The tunable filter consists of a polygon scanner and a grating in Littrow telescope-less configuration. The swept laser generates greater than 54-m W peak output power and up to 33-k Hz sweep rate with a sweep range of 150 nm centered at 1155 nm. The effects of injection current and sweep rate on the sweep performance of the swept laser are studied.     

亚音速轴流风扇后掠叶片定子与湍流互作用宽频辐射噪声预报

针对亚音速轴流风扇后掠叶片定子的宽频辐射噪声问题,介绍并推导了叶栅宽频辐射声功率计算公式,通过该公式计算后掠叶片定子的宽频辐射声功率级,并从湍流入流和叶栅响应的角度揭示后掠角对定子辐射噪声的影响机理。在此基础上,考虑到实际风扇定子工作在转子尾流中的情况,采用Gauss尾流模型模拟转子尾流,建立转子尾流湍流波数谱模型,推导得到定子叶片与转子尾流互作用的宽频辐射声功率计算公式。通过与NASA风扇试验模型对比得到,考虑转子尾流的定子叶栅宽频辐射声功率计算公式能够较好的预报后掠定子宽频辐射声功率。最后,针对试验风扇模型,分析叶片安装角、叶片弦长对后掠叶片定子辐射噪声的影响。      

掠效应对高负荷跨音转子性能的影响

本文对一高负荷跨音转子采用掠技术进行了改型设计,并通过数值模拟对原型以及前、后掠转子分别进行了流场分析。结果发现掠叶片效率和压比与原型叶片相差不大,但是前掠叶型的失速裕度得到了大幅提高。同时前掠叶型的堵塞流量比原始叶型增大,而后掠叶型却明显减小。叶片采用掠之后一方面前缘位置变化所引起的径向压力输运改变了入口来流条件,另一方面气动掠还直接影响到了叶片吸力面附面层内低能流体的径向输运以及在叶尖区域的集聚,从而使流场内部的激波强度及相对位置明显变化,并最终导致叶片不同叶高载荷分布规律的改变。     

后掠叶片锯齿尾缘宽频噪声实验研究

本文采用线性传声器阵列分别对具有常规尾缘及锯齿形尾缘的后掠叶片的尾缘噪声进行了实验测量;运用CLEAN-SC数据处理方法精确地识别出叶片尾缘噪声的声学参数.并且基于多组实验结果的对比,深入研究了不同的尾缘锯齿长度、周期、几何比例对后掠叶片尾缘噪声降噪效果的影响.实验结果表明:在低湍流度、自由来流情况下,在总声压级降噪方...     

The influence of magnetic field swept rate on the ultrasonic propagation velocity of magnetorheological fluids

Structure of magnetorheological (MR) fluids depends on the strength of the magnetic field applied and on the mode of its application. The ultrasonic wave propagation velocity changes under the effect of an external magnetic field as a result of formation of clusters arranged along the direction of the field in the MR fluids. Therefore, we propose a qualitative analysis of these clustering structures by measuring properties of ultrasonic propagation. Since the MR fluids are opaque, the non-contact inspection using this ultrasonic technique can be very useful. In this study, we measured ultrasonic propagation velocity in MR fluid influenced by an external magnetic field for different swept rate precisely. With increasing magnetic field intensity, the changes of the ultrasonic wave velocity are more pronounced. Sedimentation effect takes place in certain time for different swept rate due to magnetic particle size and it follows linear relationship in log scale. Significant differences of the ultrasonic wave velocity are established between the case when the field is swept at a constant rate and the case when it is stepped up.     

60 K脉冲管制冷机的最优设计计算

本文应用修正的一维数值计算模型对一扫气体积为10cm3的线性压缩机驱动的脉冲管制冷机进行了最优设计计算,计算结果表明10 cm3的线性压缩机可达到60 K时2 W的制冷量水平,并提供了三种供实验研究用的脉冲管制冷机尺寸.     

Swept source optical coherence tomography based on non-uniform discrete fourier transform

A high-speed high-sensitivity swept source optical coherence tomography （SSOCT） system using a high speed swept laser source is developed. Non-uniform discrete fourier transform （NDFT） method is introduced in the SSOCT system for data processing. Frequency calibration method based on a Mach-Zender interferometer （MZI） and conventional data interpolation method is also adopted in the system for comparison. Optical coherence tomography （OCT） images from SSOCT based on the NDFT method, the MZI method, and the interpolation method are illustrated. The axial resolution of the SSOCT based on the NDFT method is comparable to that of the SSOCT system using MZI calibration method and conventional data interpolation method. The SSOCT system based on the NDFT method can achieve higher signal intensity than that of the system based on the MZI calibration method and conventional data interpolation method because of the better utilization of the power of source.     

On the measurement of frequency-dependent ultrasonic attenuation in strongly heterogeneous materials

This paper deals with the measurement of frequency-dependent ultrasonic attenuation in strongly heterogeneous materials, such as cementitious materials. To improve the measurement of this parameter on this kind of materials, a linear swept–frequency signal is used to drive an emitter transducer to conduct a through-transmission inspection in immersion. To filter out undesirable frequency content, time–frequency filtering and detection process are performed. The use of this method has been compared with two excitation techniques, the broadband and the narrowband pulses. The results obtained using the swept–frequency excitation together with the time–frequency filtering, allows the determination of the attenuation curves with high accuracy over a wide frequency range without the need for complicated equipment, and improves the effective bandwidth by using a unique pair of transducers.     

On the dynamics of superfluid vorticity in non-dissipative processes

We investigate the consequences of the possible existence of superfluid vorticity on the Landau two-fluid equations. Assuming a conservation law for superfluid circulation, we show that in non-dissipative situations, the superfluid vorticity is swept along by the normal fluid.     

On the upper pressure limit for the efficient operation of a plasma focus device

We report the observation that the neutron yield (as a function of pressure) in a plasma focus device drops for high pressures, when the energy available becomes insufficient to fully ionize the gas swept during the coaxial propagation.     

线性扫频影响超短光脉冲远域衍射场分布的理论分析

本文分析了具有线性扫频高斯型超短光脉冲衍射场的能量分布,教学计算结果显示了线性扫频对衍射场的影响.通过衍射分析可以获得光脉冲的信息.     

Fourier transform properties of acousto-optic lens

A rf pulse of 4 μs swept linearly over 10 MHz, about a center frequency of 100 MHz, has been compressed to 110 ns. Fourier and Mellin transforms property of the surface acousto-optic lens has been discussed.     

后掠机翼的横流不稳定性分析及转捩预测

后掠机翼边界层的流动稳定性及转捩对翼型的设计及优化有着重要的参考价值,而横流失稳是引起后掠机翼边界层转捩的关键因素之一.以NLF（2）-0415翼型为研究对象,采用三维可压缩Navier-Stokes方程并结合γ-Re_θt转捩模式计算了展向无限长后掠机翼的基本流场.由于原始γ-Re_θt模式只能预测流向边界层转捩,因此在原始转捩模式中添加横流间歇因子项,进而对复杂构型进行横流不稳定性转捩预测.计算结果显示,利用改进后γ-Re_θt转捩模式预测得到的后掠翼型的转捩位置与实验数据吻合较好,证明了修正的转换模式的合理性和实用性.      

应用核磁共振进行聚驱后泡沫驱油特性研究

采用并联岩心进行聚驱后泡沫驱油实验,利用核磁共振技术,对驱替后岩心的不同直径孔隙内的流体分布进行了研究,得到了水驱、聚合物驱、泡沫驱替阶段的驱出油的孔径范围以及剩余油分布.实验结果表明,与水驱和聚合物驱相比,泡沫驱增大了波及的孔径的范围.泡沫可以在水驱和聚驱易发生窜流的大孔径通道形成封堵,从而波及到了水驱和聚驱未波及到的孔径,不但大幅度的提高了低渗岩心的采收率,也驱出了部分高渗岩心的小孔径的油.     

两类非对称涡流动所诱导的摇滚运动

文章详细讨论了两类非对称涡流动诱发的模型摇滚运动.第1类是针对旋成体机身组合体模型, 其摇滚运动是由前体非对称涡流动诱发的, 运功形态呈现不确定性, 由模型头尖部的扰动触发形成.文章提出了快速旋转头尖部扰动的控制技术, 以抑制该类模型的大攻角摇滚运动.第2类是针对非常规机身的组合体模型, 其摇滚运动的主控流动是非常规机身和机翼的前缘分离涡流动, 这些流动是由组合体模型的边界条件确定的, 从而运动形态具有很好的确定性.所以, 这类模型的自由摇滚运动必须通过改变边界条件来改变诱发摇滚运动的流动, 以达到抑制模型自由摇滚运动的目的.最后, 文章还讨论了这类运动是由非对称的机翼涡涡强主控的.