共查询到20条相似文献,搜索用时 426 毫秒
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《中国航空学报》2021,34(7):85-113
Gas turbines have been used extensively for aircraft and marine propulsions as well as land-based power generation because of their high thermal efficiency and large power to weight ratios. To further increase the thermal efficiency, numerous prior researches on gas turbine blade internal cooling have been intensively carried out, majorly under stationary conditions. However, the stationary studies neglect the effects of Coriolis and buoyancy forces, which should change the velocity, turbulence and temperature distribution under rotating conditions. To elucidate the rotational effects on gas turbine internal cooling, the extensive results collected from recent investigations are discussed, which include the rotation and buoyancy effects on the rib turbulated cooling, pin fin cooling, jet impingement cooling, dimple/protrusion cooling, latticework cooling as well as swirl cooling. The rotational effects on the friction factors and the most employed experimental and numerical methods are also presented. Moreover, recommendations for future research are outlined. Therefore, this review article provides extensive literature information for the design of the next-generation high-efficiency internal cooling for rotating turbine blades. 相似文献
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背景对目标红外辐射测量影响的实验研究 总被引:2,自引:0,他引:2
在排气引射红外抑制系统的实验研究中, 通过对目标背景的各种处理方法、实验对比及分析, 了解背景对目标红外辐射特性测量的影响规律。实验结果表明:在大背景小目标情况下, 必须十分注意对背景进行遮挡和冷却处理。在选择遮挡材料时, 如果被遮挡部位处于高温部件的直接辐射场中, 则应选用表面发射率高的板材, 否则应选用高反射板材。遮挡板的定向应使其板面垂线与探测器轴线有较大夹角。 相似文献
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L. O’C. Drury D.E. Ellison F.A. Aharonian E. Berezhko A. Bykov A. Decourchelle R. Diehl G. Meynet E. Parizot J. Raymond S. Reynolds S. Spangler 《Space Science Reviews》2001,99(1-4):329-352
The main features of cosmic-ray source models and acceleration processes are reviewed, with special emphasis on the possible observational tests, through both composition analysis and multi-wavelength studies of supernova remnants. Non-linear effects in the context of supernova-induced diffusive shock acceleration are discussed, as well as collective acceleration effects induced by multiple supernova explosions inside superbubbles. 相似文献
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Synthetic Aperture Imaging Radar and Moving Targets 总被引:7,自引:0,他引:7
This paper considers the effects of slowly moving targets as they appear in the output of an airborne coherent side-looking synthetic aperture imaging radar. The image of a moving reflector is described, and two approaches to airborne moving target indication (AMTI) are summarized. It is shown that the effects of target movement are decreased as the radar scan rate is increased, and are increased as the (Doppler processed) compression ratio is increased. 相似文献
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大展弦比复合材料机翼失速颤振分析 总被引:1,自引:0,他引:1
研究了大展弦比复合材料机翼在较大迎角状态下的失速颤振特性,探讨了结构几何非线性和由复合材料剪裁产生的刚度耦合效果对机翼失速颤振特性的影响.首先,将复合材料机翼建模为转角和位移均可为有限值的非线性薄壁单闭室截面Euler梁,并在综合考虑结构几何非线性、气动非线性和材料各向异性对机翼运动状态的影响的基础上,建立机翼的运动微分方程.然后,使用小扰动分析的方法得到机翼在平衡位置附近的振动方程,采用ONERA半经验的非定常失速气动力模型,获得机翼在平衡位置附近的非线性失速颤振分析方程.最后,利用谐波平衡法求解并判定机翼颤振稳定性.通过算例,首先验证了算法的正确性,然后研究了几何非线性对失速颤振的影响,并讨论不同的复合材料铺层方式导致机翼失速特性的改变. 相似文献
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本文讨论了关于风洞侧壁效应原理的几种不同的理论解释,即尾涡模型,位移效应模型和前缘马蹄涡模型。从实验观察和基本原理两个方面对上述不同解释进行了考察。指出原有理论存在不同程度的缺陷和片面性。在此基础上对侧壁效应原理提出了较为全面的解释。 相似文献
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以二维高超声速进气道GK01[1]为计算模型,对进气道进行无粘、粘性以及边界层分离控制方法数值研究.结果发现,利用文中设计的壁面开缝措施可以有效减小甚至消除激波/边界层干扰带来的边界层分离现象,降低粘性效应造成的负面影响;相对开缝前,开缝措施在设计点和非设计点均能明显提高进气道的总压恢复系数和动能效率,而对流量捕获系数的影响很小.同时文中给出了开缝措施在非设计点下对进气道性能指标的影响规律. 相似文献
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随着技术的进步,越来越多的现代高技术航空电子系统在直升机上得到应用。在提高系统灵敏度的同时,也带来了闪电间接效应防护问题。在分析闪电间接效应防护的适航要求的基础上,结合AC313型机适航验证结果,提出适航验证方法,对其它直升机闪电间接效应防护有一定的参考价值。 相似文献
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B. Heber A. Raviart C. Paizis W. Dröge R. Ducros P. Ferrando H. Kunow R. Müller-Mellin C. Rastoin K. Röhrs H. Sierks G. Wibberenz 《Space Science Reviews》1995,72(1-2):391-396
The cosmic ray flux observed with the Kiel Electron Telescope on board the ULYSSES spaceprobe varies with solar activity as well as with heliospheric position. Determination of the latitudinal gradients requires a careful analysis of the influences of the current sheet tilt angle, the number of major solar flares, interplanetary shocks and interaction regions evolving in the expanding solar wind. In this paper we concentrate on nuclei with rigidity above 1 GV. We discuss the effects of the variable solar activity in the declining phase of the present solar cycle and the variation with radial distance as a basis for separating latitudinal effects. We show that during this phase of the solar cycle modulation of GV nuclei is ordered by temporal evolution, radial distance and negligible latitudinal effects even at latitudes between 30° and 50° South. 相似文献
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基于常规多普勒滤波器组结构的合成宽带距离像性能分析 总被引:3,自引:2,他引:1
为了消除散布效应对宽带信号的不利影响,可以利用多个窄带信号合成宽带信号;同时,通过在子带内处理相干脉冲串,可进行杂波抑制、目标速度估计和区分不同速度的目标。然而,在子带内分别使用常规多普勒滤波器组,会引进多普勒散布效应所造成的输出失配误差,从而造成合成距离像的失真。分析了多普勒散布效应与子带常规多普勒滤波器组输出失配之间的关系,推导了运动目标通过滤波器组后所成高分辨距离像的距离走动公式,给出了适合子带常规多普勒滤波器组的目标速度临界值。仿真实验验证了以上结论。 相似文献
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某型航空发动机空中起动供油规律的研究 总被引:5,自引:3,他引:2
研究某型航空发动机空中起动困难问题,现有自动起动器没有考虑飞行高度对供油规律的影响,发动机在空中起动时存在富油状态.分析了影响起动供油规律的因素,在现有自动起动器结构基础上,设计了高空修正模块来补偿飞行高度对供油规律的影响.建立了自动起动器的数学模型,对改进的自动起动器进行了仿真分析和试验.仿真结果和试验验证了改进方案的可行性,与地面起动相比,空中起动的供油量随着飞行高度的增加而降低.采用改进的空中起动供油规律可补偿飞行高度对供油特性的影响,解决发动机空中起动时的富油状态问题. 相似文献
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空间用聚四氟乙烯材料的原子氧、温度、紫外辐射效应的试验研究 总被引:5,自引:0,他引:5
在 IFM原子氧剥蚀效应地面模拟设备中对空间常用材料聚四氟乙烯进行了原子氧剥蚀效应试验,试样温度升高对原子氧效应的影响以及原子氧与紫外辐射复合效应试验,对试验前后试样的质量及表面形貌进行了比较,得出了材料在设备中的反应特点以及温度升高、紫外辐射对材料的原子氧效应的影响规律。对原子氧与材料的反应机理也做了相应的分析。同时还测量比较了原子氧暴露试验前后、原子氧与紫外辐射复合作用前后试样的反射率、透射率等光学性质。 相似文献
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以开放经济与贸易的理论模型为基础,对工资差距、失业和环境污染等问题进行综合考量.认为要素禀赋(如非熟练劳动力的数量、熟练劳动力的数量)和相关变量(如城市工业部门的固定工资、对进口工业品的关税政策)的变化会对工资差距、失业和环境产生十分复杂的影响.文章对这些影响进行了系统的理论分析,为制订解决这些问题的经济政策提供理论观点和参考意见. 相似文献
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关于剩磁对卫星姿态确定与控制影响的研究 总被引:5,自引:3,他引:2
讨论了稳态剩磁对地磁姿态确定与控制系统的性能的影响。对某些卫星来说,星上的直流电设备单元会产生一个支配性的稳定磁场。文中提出一个姿态确定滤波器对剩磁场的影响进行了估计,然后从剩磁矩指向、大小及伸杆长度3方面分析了剩磁干扰力矩对姿态控制精度的影响。通过计算机仿真发现:该滤波器能有效消除剩磁场对姿态确定的影响;不同指向的剩磁矩令三轴控制精度出现较大的起伏,而不断增大的剩磁量则使控制偏差呈正比例增大,伸杆长度的影响却很微小。 相似文献
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Parametric study of turbine NGV blade lean and vortex design 总被引:1,自引:1,他引:0
《中国航空学报》2016,(1):104-116
The effects of blade lean and vortex design on the aerodynamics of a turbine entry nozzle guide vane (NGV) are considered using computational fluid dynamics. The aim of the work is to address some of the uncertainties which have arisen from previous studies where conflicting results have been reported for the effect on the NGV. The configuration was initially based on the energy efficient engine turbine which also served as the validation case for the computational method. A total of 17 NGV configurations were evaluated to study the effects of lean and vortex design on row efficiency and secondary kinetic energy. The distribution of mass flow ratio is introduced as an additional factor in the assessment of blade lean effects. The results show that in the turbine entry NGV, the secondary flow strength is not a dominant factor that determines NGV losses and therefore the changes of loading distribution due to blade lean and the associated loss mecha-nisms should be regarded as a key factor. Radial mass flow redistribution under different NGV lean and twist is demonstrated as an addition key factor influencing row efficiency. 相似文献