Experimental investigation and correlation development of jet impingement heat transfer with two rows of aligned jet holes on an internal surface of a wing leading edge

Extensive experimental studies on the heat transfer characteristics of two rows of aligned jet holes impinging on a concave surface in a wing leading edge were conducted, where50000 Rej 90000, 1.74 H/d 27.5, 66° a 90°, and 13.2 r/d 42.03. The finding was that the heat transfer performance at the jet-impingement stagnation point with two rows of aligned jet holes was the same as that with a single row of jet holes or the middle row of three-row configurations when the circumferential angle of the two jet holes was larger than 30°. The attenuation coefficient distribution of the jet impingement heat transfer in the chordwise direction was so complicated that two zones were divided for a better analysis. It indicated that： the attenuation coefficient curve in the jet impingement zone exhibited an approximate upside-down bell shape with double peaks and a single valley; the attenuation coefficient curve in the non-jet impingement zone was like a half-bell shape, which was similar to that with three rows of aligned jet holes; the factors,including Rej, H/d and r/d, affected the attenuation coefficient value at the valley significantly.When r/d was increased from 30.75 to 42.03, the attenuation rates of attenuation coefficient increased only by 1.8%. Consequently, experimental data-based correlation equations of the Nusselt number for the heat transfer at the jet-impingement stagnation point and the distributionof the attenuation coefficient in the chordwise direction were acquired, which play an important role in designing the wing leading edge anti-icing system with two rows of aligned jet holes.

The relation between black hole masses and Lorentz factors of the jet components in blazars

We explore the relationship between black hole mass （MBH） and the motion of the jet components for a sample of blazars. The Very Long Baseline Array （VLBA） 2 cm Survey and its continuation： Monitoring of Jets in active galactic nuclei （AGNs） with VLBA Experiments （MOJAVE） have observed 278 radio-loud AGNs, of which 146 blazars have reliable measurements of their apparent velocities of the jet components. We calculate the minimal Lorentz factors for these sources from their measured apparent velocities, and their black hole masses are estimated with their broad-line widths. A significant intrinsic correlation is found between black hole masses and the minimal Lorentz factors of the jet components. The Eddington ratio is only weakly correlated with the minimal Lorentz factor, which may imply that the Blandford-Znajek （BZ） mechanism may dominate over the Blandford-Payne （BP） mechanism for the jet acceleration （at least） in blazars.

Rapid manufacturing of SiC molds with micro-sized holes using abrasive water jet

Silicon carbide (SiC) is highly wear resistant with good mechanical properties, including high temperature strength, excellent chemical resistance, and high thermal conductivity and thermal shock resistance. SiC molds, which can be produced with diverse microstructural features, are now widely used in glass molding owing to their excellent characteristics, and also have potential applicability in IT industries. SiC molds are traditionally fabricated by silicon micromachining or dicing. The fabrication cost of silicon micromachining is very high, however, because several expensive masks are needed. Furthermore, the fabrication time is very long. Meanwhile, it is difficult to make micro-patterned molds with arbitrary shapes using dicing saws. Abrasive water jet (AWJ) is widely applied to cut and drill very brittle, soft and fibrous materials. It offers high energy density, the absence of a heat affected zone(HAZ), high performance, and an environment friendly process. In spite of these advantages, micro-hole drilling via conventional AWJ processing suffers from notable shortcomings. We proposed a new abrasive supplying method of AWJ. The proposed method reduces frosting phenomena, and provides micro-machining of AWJ. The characteristics of a hole machined was investigated by the proposed AWJ process according to the ratio of water and abrasives. With the optimal experimental conditions, 3×3 array SiC molds with the diameter of 700 μm and depth of 900 μm were successfully manufactured.

Jet-dominated quiescent state in black hole X-ray binaries: the cases of A0620–00 and XTE J1118+480

The radiative mechanism of black hole X-ray transients （BHXTs） in their quiescent states （defined as the 2-10 keV X-ray luminosity ≤ 10^34 erg s-1） remains unclear. In this work, we investigate the quasi-simultaneous quiescent state spectrum （including radio, infrared, optical, ultraviolet and X-ray） of two BHXTs, A0620-00 and XTE J1118＋480. We find that these two sources can be well described by a coupled accretion - jet model. More specifically, most of the emission （radio up to infrared, and the X-ray waveband） comes from the collimated relativistic jet. Emission from hot accretion flow is totally insignificant, and it can only be observed in mid-infrared （the synchrotron peak）. Emission from the outer cold disk is only evident in the UV band. These results are consistent with our previous investigation on the quiescent state of V404 Cyg and confirm that the quiescent state is jet-dominated.

Dynamics and collisions of episodic jets from black holes and accretion disk systems

In many astrophysical black hole systems, episodic jets of plasma blobs have been observed, which are much faster and more powerful than continuous jets. A magnetohydrodynamical model was proposed by Yuan et al. to study the formation of episodic jets in Sgr A＊. By taking Sgr A＊ and a stellar mass black hole as examples, we modify the model of Yuan et al. by including the effects of relativity, and further study the relativistic motion and expansion of episodic jets of plasma blobs. Then we study the collision between two consecutive ejections in the modified model, and calculate the magnetic energy released in the collision. Our results show two consecutive blobs can collide with each other, and the released magnetic energy is more than 1050 erg, which supports the idea that a gamma-ray burst is powered by the collision of episodic jets, as suggested by Yuan ＆ Zhang.

波流环境中多孔射流三维数值模拟

建立了波流环境中多孔射流的三维大涡数学模型,探讨了波流共同作用下多孔射流的扩散和稀释机制,分析了孔间距对双孔射流、射流与环境水体相互作用的影响,并给出了最优相对孔间距。模拟结果表明:在波谷相位时刻,由于横流与波浪相互作用强烈,流场内的三维涡旋结构丰富、尺度较大、数目众多,有利于射流与环境水体、射流与射流之间的掺混,这是波流环境比单一横流环境中多孔射流运动扩散效果更佳的主要原因;随着孔间距的增大,双孔射流之间的相互作用慢慢削弱,而射流与环境水体之间的相互作用却在不断增强;双孔射流在孔间距为7.0倍管口直径时扩散效果最好。

燃烧室百叶与双排孔冷气对透平端壁冷却性能影响研究

针对燃烧室与透平冷气掺混导致实际二次流发展及端壁冷却性能偏离设计值的问题,综合考虑燃烧室百叶冷气尾迹与双排孔射流,数值研究了多源冷气射流在燃烧室与透平交界区的掺混机制,分析了其对透平静叶端壁气膜冷却与流动特性的影响规律。研究结果表明:空腔涡卷吸大部分百叶冷气,并跨越双排孔冷气向下游发展,马蹄涡卷吸限制大部分双排孔冷气,并向空腔涡外侧发展;当双排孔冷气吹风比M_h=0.5,1.0较小时,马蹄涡导致冷气形成楔形高冷效区域,空腔涡的附着侧和分离侧分别产生了高、低冷效区,随着百叶冷气吹风比M_l的增加,空腔涡强度显著降低,导致位于楔形中心的分离侧冷却效率有所提升;当双排孔冷气吹风比M_h为1.5时,双排孔冷气部分跨越马蹄涡,静叶端壁可实现完全冷气覆盖,此时百叶冷气吹风比M_l从0.5增加到1.5,静叶端壁平均冷却效率可从0.4提升到0.63。该研究为考虑燃烧室与透平交界区实际流动掺混情况的静叶端壁冷却结构与布局设计提供理论基础。

变径孔射流冲击冷却的流动与传热特性数值研究

采用数值方法开展了变径孔射流冲击冷却的流动与传热性能研究。设计了3种变径孔射流冲击冷却结构,即收缩孔、直孔、扩张孔。对比了不同雷诺数情况下3种孔型射流冲击冷却的流动与传热特性。分析了雷诺数和孔型对射流冲击冷却流动性能、传热性能和综合热力性能的影响。拟合得到了不同孔型冲击冷却的平均努塞尔数、压力损失系数和综合热力系数有关于雷诺数的经验关联式。结果表明:与直孔冲击冷却相比,雷诺数为6000~30 000时,收缩孔冲击冷却的压力损失系数增加了约16.67倍~21.09倍,靶面平均努塞尔数提升了约0.96倍~1.85倍;扩张孔冲击冷却的压力损失系数降低了约22.55%~33.68%,靶面平均努塞尔数降低了约5.62%~10.85%。在3种孔型中,收缩孔冲击冷却的传热性能最优、流动性能最差,直孔冲击冷却的传热性能和流动性能都处于中等水平,而扩张孔冲击冷却的传热性能最差、流动性能最好。当雷诺数小于24 000时,扩张孔冲击冷却的综合热力性能最优,其次为直孔冲击冷却,而收缩孔冲击冷却的综合热力性能最差。当雷诺数大于等于24 000时,3种孔型冲击冷却的综合热力性能很接近。研究结果可以为未来先进燃气轮机内部变径孔冲击冷却的设计提供一定的参考。

高压气体双孔浸没射流振荡频率特性研究

在沸水堆或小型堆中一般将抑压水池作为气体排放的热阱以实现安全壳压力的有效控制。基于这一背景,本文在不同过冷度下对高压气体双孔浸没射流振荡主频特性进行了一系列实验研究,其中不凝性气体份额为0.0~0.4,孔间距范围为1.5 d~3 d。实验结果表明,无论是纯蒸汽还是混合气,在双孔射流时两股气羽均表现出向中间汇聚的形态,甚至汇聚到一起形成联合射流,相较单孔射流而言双孔射流气羽尺度增大冷凝时间延长,所以其振荡主频更低。分析射流参数影响发现,纯蒸汽射流振荡主频随过冷度和孔间距的增加而增加。同时本文总结振荡主频影响规律提出了纯蒸汽射流主频的预测关系式,预测精度在-15%~20%之间。混合气体射流时(纯蒸汽+不凝性气体)振荡主频随过冷度和孔间距的增加而增加,与纯蒸汽射流主频变化规律一致。值得注意的是,混合气射流相较纯蒸汽而言振荡主频更低,并且主频随不凝气份额增加而降低。

带同轴引气激光制孔中的气动特性分析

针对锥形激光加工器在航空发动机热部件冷却孔加工过程中的吹渣效果,研究了射流冲击孔板附近的流场特性及其影响因素。针对同轴高压气体撞击带盲孔平板的射流结构,采用数值模拟方法,分析了不同进气压力p_(int)(0.2~1.5 MPa)、射流间距H/De(3.6,5.6,7.6)和冲击角度α(30°,45°,60°,90°)对盲孔附近气体动力学性能的综合影响。研究结果表明,当H/De为3.6时,随进气压力的增大,盲孔附近的气体动力学性能呈现先逐步提高后剧烈下降的趋势,较好工作压力为1 MPa;当射流间距H/De达到5.6及以上时,适当地增大喷嘴压力可以提高盲孔附近气流的气动水平,但提升有限。随着冲击角度α减小,盲孔内流出质量流量逐渐增大,α为30°时较垂直射流提升约11倍,但在冲击表面上气体的剪切流动随冲击角度减小逐渐变弱。

随钻选择性扩眼器锥直型水眼液力特性研究

在随钻扩眼技术中,扩眼器的射流效率决定了整个扩眼技术的效率,对整个扩眼技术应用极为重要。针对扩眼器和扩眼器刀翼水眼的液力特性,建立了其物理有限元模型。通过分析可知,射流可以起到清洗岩石切割和冷却刀翼的作用,扩眼器刀翼水眼的几何结构对射流性能有重要影响。为了优化扩眼器刀翼水眼射流性能,提出了将锥直型喷嘴应用于扩眼器刀翼水眼,对其进行了优化。该研究可为扩眼器刀翼水眼结构参数的优化设计提供理论指导,对提高侧钻完井质量、推广侧钻改造技术具有重要意义。

反循环气动潜孔锤进气端分流引射接头设计及结构参数分析

为解决反循环气动潜孔锤在钻进过程中岩石重复破碎及排渣效率低下的问题,笔者基于NGQ-320反循环气动潜孔锤设计了进气端分流引射接头。该接头可实现潜孔锤供气量的动态调节,其引射结构可以将部分压缩气体引入中心通道,对井底流场产生泵吸作用的同时改善冲击机构的动力供给;同时采用CFD技术研究了分流引射接头局部流场,分析了喷射孔夹角、喷射孔开口深度、喷射孔直径和喷射孔偏转角度等参数对中心通道抽吸性能的影响,确定了各项结构参数的较优取值。结果表明,分流引射接头在喷射孔开口深度320~330 mm、喷射孔夹角30°~35°、喷射孔直径12 mm、喷射孔偏转角11°~13°的情况下具有较好的抽吸性能。

空穴射流清垢技术在德苏输油管线的应用

因油田产量递减,德苏输油管道采用含水油外输,为减缓苏一联污水站运行压力,采用高温低输量的运行模式,导致管道结垢严重,管道有效通径缩减,严重影响管道安全平稳运行。本次利用空穴射流清垢技术成功实现德苏输油管道全线清管通球,有效清除了管线内结垢,降低了德二联外输压力。清垢过程具有安全、速度快、无环境污染等优点,对海拉尔油田输油管道运行管理具有十分重要意义。

海底电缆覆盖物清理的移动射流过程仿真分析

在实际工况中,高压喷嘴存在横向移动的速度,使得射流对土体的冲埋深度难以预测,导致海缆表面覆盖物清理不完全。针对此问题,建立了优化后的流场与冲埋深度预测理论模型,利用数值仿真对模型进行了验证。首先,建立了一种喷嘴流场优化模型,阐述了冲埋深度的预测方法;其次,建立了水射流破土数值仿真模型,选取射流压强、喷嘴直径、喷嘴横移速度以及土壤剪切强度4种控制参数,分析了不同参数对冲埋深度的影响。结果表明,随着射流压强、喷嘴直径的增大,冲坑深度逐渐增大;随着喷嘴横移速度和土体剪切强度的增加,冲坑深度逐渐减小。最后,理论结果和仿真结果进行对比,两者误差在允许范围之内。该模型可在一定程度上解决冲埋深度难以预测的问题,可为工程应用提供指导。

嵌岩低桩承台锁口钢管桩围堰设计与施工技术

昌九高铁扬子洲赣江公铁大桥西支主桥为(48+144+320+144+48)m无砟轨道钢箱桁组合梁斜拉桥。桥塔墩位于通航河道内,桥位处河床覆盖层浅,基岩强度高,基础由大直径钻孔桩和矩形嵌岩低桩承台组成,承台采用锁口钢管桩围堰施工方案。G33号主墩围堰平面设计尺寸54.56 m×28.52 m,锁口钢管桩采用Q345B材质∅1020 mm螺旋钢管,长28 m,钢管桩之间采用C-T形锁扣连接;围堰设置4层内支撑,单层内支撑设3道对撑,内支撑四角设型钢斜撑;基底设置混凝土垫层参与围堰结构受力。围堰采用XR360旋挖钻机在岩层中引孔,孔内换填细砂后插打钢管桩,钢管桩壁内、外两侧换填砂采用高压旋喷注浆加固。围堰设置智能化监测系统,对围堰受力、变形等进行实时动态监控。实践证明,该桥围堰结构安全可靠、止水效果良好、施工快捷高效。

水平旋喷桩在风积沙隧道洞口段的应用分析

风积沙作为抗剪能力弱、黏聚力低、自稳能力差的土体,隧道开挖时围岩变形难以控制。水平旋喷桩具有高效、环保、经济等独特优势,已广泛应用于风积沙隧道中,属于一种预加固施工技术。为了解风积沙地层隧道失稳变形特征和预加固控制效果,本文依托拉林铁路德吉隧道采用水平旋喷桩对风积沙隧道进行超前支护,并取得了不错的成效,积累了丰富的施工经验。

高压旋喷型圆形复合支护桩在深厚填土质斜坡工程中的应用及探讨

以某市政道路项目为实例,阐述了普通圆形支护桩在深厚填土质斜坡实施过程中遇到的刚度不足及塌孔等问题,提出了一种较为稳定可靠的高压旋喷圆形复合支护桩。该结构主要由高压旋喷复合土及钢筋混凝土圆形支护桩组成,为桩土复合支护结构,由高压旋喷固结体及圆形支护桩一起承担水平土压力,具有防止垮孔,提高支护桩刚度及桩周土体物理力学指标等优点。在分析复合型支护桩受力特征基础上,通过理论推导,得到桩截面刚度提高公式。应用结果表明:采用高压旋喷型圆形复合支护桩可以有效提高桩身刚度,减小支护桩使用阶段水平位移,同时解决了桩基施工过程中垮孔问题,对填土斜坡上的支护桩有一定的普适性。

Does black hole spin play a key role in the FSRQ/BL Lac dichotomy?

Blazars are characterized by large intensity and spectral variations across the electromagnetic spectrum It is believed that jets emerging from them are almost aligned with the line-of-sight. The major- ity of identified extragalactic sources in γ-ray catalogs of EGRET and Fermi are blazars. Observationally, blazars can be divided into two classes： fiat spectrum radio quasars （FSRQs） and BL Lacs. BL Lacs usually exhibit lower γ-ray luminosity and harder power law spectra at γ-ray energies than FSRQs. We attempt to explain the high energy properties of FSRQs and BL Lacs from Fermi γ-ray space telescope observations. It was argued previously that the difference in accretion rates is mainly responsible for the large mismatch in observed luminosity in ＂7-ray. However, when intrinsic luminosities are derived by correcting for beaming effects, this difference in 7-ray luminosity between the two classes is significantly reduced. In order to ex- plain this difference in intrinsic luminosities, we propose that spin plays an important role in the luminosity distribution dichotomy of BL Lacs and FSRQs. As the outflow power of a blazar increases with increasing spin of a central black hole, we suggest that the spin plays a crucial role in making BL Lac sources low luminous and slow rotators compared to FSRQ sources.

Features of Ozone Mini-Hole Events over the Tibetan Plateau

Based on TOMS total ozone data and SCIAMACHY ozone profile data, climatology of the ozone minihole events over the Tibetan Plateau and ozone vertical structure variations during an ozone mini-hole event in December 2003 are analyzed. The analyses show that before 1990 ozone mini-hole events only occurred in November-December of 1987 but that the number of events increases after 1990. These events only occur from October through February, with maximum occurrence frequency in December. During the event in December 2003, the decrease in total ozone of over 20% is mainly caused by the ozone loss in the upper troposphere and lower stratosphere region due to the horizontal transport of low ozone from the lower latitude subtropics and the uplift of low ozone from the lower troposphere over the Tibetan Plateau.

A disk-corona model for the low/hard state of black hole X-ray binaries

A disk-corona model for fitting the low/hard（LH）state of the associated steady jet in black hole X-ray binaries（BHXBs）is proposed based on the large-scale magnetic field configuration that arises from the coexistence of the Blandford-Znajek（BZ）and Blandford-Payne（BP）processes,where the magnetic field configuration for the BP process is determined by the requirement of energy conversion from Poynting energy flux into kinetic energy flux in the jet.It is found that corona current is crucial to guarantee the consistency of the jet launching from the accretion disk.The relative importance of the BZ and BP processes in powering jets from black hole accretion disks is discussed,and the LH state of several BHXBs is fitted based on our model.In addition,we suggest that magnetic field configuration can be regarded as the second parameter for governing the state transition of BHXBs.