气量分配对轴径向旋流杯燃烧室贫熄边界的影响

针对轴径向旋流杯燃烧室,研究了头部进气面积及主燃孔布局对此类燃烧室贫熄特性的影响.实验结果表明:减小一级轴向旋流器进气面积和增加主燃孔个数对燃烧室贫熄性能有较大影响.一级进气面积减小20%可拓宽贫熄边界9.7%;增加主燃孔为4个时,燃烧室贫熄边界变宽约7.6%.此外,增加一级进气面积20%,改变二级进气面积20%及改变主燃孔个数为2个等情况对燃烧室贫熄边界影响较小.      

High energy radiation from the direction of the galactic black hole Sgr A

X-ray observations indicate that the Galactic black hole Sgr A^∗ is inactive now, however, we suggest that Sgr A^∗ can become active when a captured star is tidally disrupted and matter is accreted into the black hole. Consequently the Galactic black hole could be a powerful source of relativistic protons with a characteristic energy ∼10⁵² erg per capture. The diffuse GeV and TeV γ-rays emitted in the direction of the Galactic Center (GC) are the direct consequences of p–p collisions of such relativistic protons ejected by very recent capture events occurred ?10⁵ yr ago. On the other hand, the extended electron-positron annihilation line emission observed from GC is a phenomenon related to a large population of thermalized positrons, which are produced, cooled down and accumulated through hundreds of past capture events during a period of ∼10⁷ yr. In addition to explaining GeV, TeV and 511 keV annihilation emissions we also estimate the photon flux of several MeV resulting from in-flight annihilation process.     

Theoretical study of flow ripple for an aviation axial-piston pump with damping holes in the valve plate

Based on the structure of a certain type of aviation axial-piston pump＇s valve plate which adopts a pre-pressurization fluid path （consisting a damping hole, a buffer chamber, and an orifice） to reduce flow ripple, a single-piston model of the aviation axial-piston pump is presented. This sin- gle-piston model comprehensively considers fluid compressibility, orifice restriction effect, fluid resistance in the capillary tube, and the leakage flow. Besides, the instantaneous discharge areas used in the single-piston model have been calculated in detail. Based on the single-piston model, a multi-piston pump model has been established according to the simple hydraulic circuit. The sin- gle- and multi-piston pump models have been realized by the S-function in Matlab/Simulink. The developed multi-piston pump model has been validated by being compared with the numerical result by computational fluid dynamic （CFD）. The effects of the pre-pressurization fluid path on the flow ripple and the instantaneous pressure in the piston chamber have been studied and opti- mized design recommendations for the aviation axial-piston pump have been given out.     

机匣内间断形深孔机械加工研究

通过优化方案自主设计了一套用于深孔加工的刀具方案,用于某发动机主机匣内部关键件凸轮轴的安装孔的加工,为系列化研制该类机型积累了加工经验.     

钉载作用下层板多孔过盈配合分析

本文利用各向异性体平面弹性理论中的复势方法,以Faber级数为工具,导出层板多孔/弹性核过盈配合在钉载作用下的级数解。     

肼推进系统管路工艺孔的一种自动焊技术

介绍了氩气保护自动堵孔焊技术及其所用设备、换气焊接系统、焊接电源等。同时给出了试样焊接、模拟实样堵焊试样的检测试验数据。介绍了焊接的质量，试验表明，各项数据全部符合设计要求。实践证明，自动堵孔焊技术是完全可行的，其设备稳定可靠，重复性好。     

跨声速叶栅通道中叶片压力面簸箕孔型气膜冷却特性

在跨声速叶栅通道内,试验研究了叶片压力面气膜冷却特性,详细地对比分析了在不同主流进口雷诺数(Re=17×105,37×105,57×105)、出口马赫数(Ma=081,091,101)及多个气膜吹风比(M=05～30)条件下的压力面簸箕孔型气膜冷却效率。试验结果表明:主流出口马赫数变化对气膜孔下游冷却效率的分布与具体数值均无影响;而主流进口雷诺数的影响较大。增大主流进口雷诺数使得气膜分离再贴附对应的吹风比相应增大,Re=17×105时在吹风比M=10时出现气膜分离与再贴附现象,而Re=37×105和Re=57×105对应的临界吹风比则分别为20和25;主流进口雷诺数越大,小吹风比下近孔区域的冷却效率越高,而在孔下游区域则相反;大吹风比下,则主流进口雷诺数越大冷却效率越小。     

Black hole accretion and X-ray spectra of QSOS

Changes in Eddington accretion ratios are thought to result in X-ray spectral index changes in Galactic binary black hole systems. Objects with higher Eddington ratios have softer X-ray spectra. Can we apply this result to much more massive black hole systems such as QSOs? If so, X-ray observations will give us valuable insight into the physics of QSOs. Among QSOs, X-ray spectral index is part of a large set of correlated optical and UV observational properties, especially optical Fe II and [O III] strengths in the Hβ region. To investigate whether this set of correlations is related to Eddington ratio, we use as probes, BALQSOs that have been suggested to be youthful super-accretors. We conducted infrared spectroscopy of the Hβ rest wavelength region for a sample of BALQSOs and compared line measurements with those for high and low redshift non-BAL QSOs. Hβ line widths and bolometric luminosity are used to calculate QSO black hole masses and Eddington ratios. Our results support the hypothesis that optical Fe II and [O III] line strengths are Eddington ratio indicators in QSO central engines. A possible explanation is that strong Fe II and weak [O III] indicate abundant cold gas that could fuel near Eddington accretion.     

The case for massive,evolving winds in black hole X-ray binaries

In the last decade, high-resolution X-ray spectroscopy has revolutionized our understanding of the role of accretion disk winds in black hole X-ray binaries. Here I present a brief review of the state of wind studies in black hole X-ray binaries, focusing on recent arguments that disk winds are not only extremely massive, but also highly variable. I show how new and archival observations at high timing and spectral resolution continue to highlight the intricate links between the inner accretion flow, relativistic jets, and accretion disk winds. Finally, I discuss methods to infer the driving mechanisms of observed disk winds and their implications for connections between mass accretion and ejection processes.     

鲁棒的结构网格自动化重叠方法

网格技术是目前数值模拟中的关键技术之一。重叠网格是一种放宽拓扑要求、减小网格生成难度的网格技术。本文以结构重叠网格为基础,分别针对挖洞、寻点以及洞面优化方法进行了研究和改进,同时完成物面网格重叠,形成了一套鲁棒的、自动化的网格重叠系统。在挖洞方面,结合“最小洞映射”方法,提出“复合式挖洞”方法,节省内存开销;在寻点方面,通过构建格心虚网格,保证搜索空间的连续性,同时结合“有效搜索”思想,排除部分对寻点无贡献的网格点,进而减少ADT叉树节点;在洞面优化上,改变填补判别法则并引入两类受保护洞内点,确保两层插值边界建立,提高鲁棒性;在物面网格重叠上,利用物面投影法完成坐标修正,实现物面附近网格流动变量的准确传递。为验证本文方法,分别对定常翼身组合体DLR-F6绕流和非定常机翼挂载分离过程进行了数值模拟,计算结果与实验结果吻合良好,表明该结构重叠网格系统对多物体间定常、非定常扰流具有较好的数值模拟能力和较高的模拟精度,具有较高的工程应用价值。