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761.
大学就业困难学生帮扶体系研究 总被引:2,自引:0,他引:2
就业是民生之本,对就业困难学生进行帮扶是高校就业工作中的重要内容。高校应充分认识对就业困难学生进行帮扶的必要性,同时应采取各种措施帮助就业困难学生顺利就业。 相似文献
762.
时媛 《西安航空技术高等专科学校学报》2014,(6):30-33
产业融合是现代产业发展的必然结果,利用2002-2007年安徽省投入产出表相关数据,结合中间投入率和中间需求率,对安徽省生产性服务业和制造业间的融合度进行测算,探究安徽省产业融合特点和规律,旨在为安徽省产业结构调整和转型升级提供科学依据。研究表明:整体制造业和生产性服务业相互依赖,融合程度在不断加深,生产性服务业的投入主要集中在劳动和资源密集型产业,对技术密集型产业的投入较低,不同生产性服务业对整体制造业的投入结构存在明显差异。 相似文献
763.
In order to improve the deposition rate and microstructure of pyrocarbon, nickel was introduced by electroplating on carbon fibers and used as a catalyst during the deposition of pyrocarbon at 1000 C using methane as a precursor gas. The distribution of nickel catalyst and the microstructure of pyrocarbon were characterized by scanning electron microscopy(SEM), energy dispersive spectroscopy(EDS), X-ray diffraction(XRD), and Raman micro-spectrometry. Results show that nano-sized nickel particles could be well distributed on carbon fibers and the pyrocarbon deposited catalytically had a smaller d002 value and a higher graphitization degree compared with that without catalyst. In addition, the deposition rate of pyrocarbon in each hour was measured.The deposition rate of pyrocarbon in the first hour was more than 10 times when carbon cloth substrates were doped with nickel catalysts as compared to the pure carbon cloths. The pyrocarbon gained by rapid deposition may include two parts, which are generation directly on the nickel catalyst and formation with the carbon nanofibers as crystal nucleus. 相似文献
764.
The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formulated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions. 相似文献
765.
In order to promote an in-depth understanding of the mechanism of leading-edge flow separation control over an airfoil using a symmetrical Dielectric Barrier Discharge(DBD) plasma actuator excited by a steady-mode excitation, an experimental investigation of an SC(2)-0714 supercritical airfoil with a symmetrical DBD plasma actuator was performed in a closed chamber and a low-speed wind tunnel. The plasma actuator was mounted at the leading edge of the airfoil.Time-resolved Particle Image Velocimetry(PIV) results of the near-wall region in quiescent air suggested that the symmetrical DBD plasma actuator could induce some coherent structures in the separated shear layer, and these structures were linked to a dominant frequency of f0= 39 Hz when the peak-to-peak voltage of the plasma actuator was 9.8 kV. In addition, an analysis of flow structures without and with plasma actuation around the upper side of the airfoil at an angle of attack of18° for a wind speed of 3 m/s(Reynolds number Re = 20000) indicated that the dynamic process of leading-edge flow separation control over an airfoil could be divided into three stages. Initially, this plasma actuator could reinforce the shedding vortices in the separated shear layer. Then, these vortical structures could deflect the separated flow towards the wall by promoting the mixing between the outside flow with a high kinetic energy and the flow near the surface. After that, the plasma actuator induced a series of rolling vortices in the vicinity of the suction side of the airfoil, and these vortical structures could transfer momentum from the leading edge of the airfoil to the separated region, resulting in a reattachment of the separated flow around the airfoil. 相似文献
766.
针对颅骨民族判别问题,提出结合颅骨形态特征与神经网络的判别方法,可以推进法医人类学的发展,加快探索民族发展历程。首先,根据颅骨形态学相关研究,提取36个维吾尔族和汉族颅骨数据的几何特征;其次,采用反向传播神经网络(BPNN)对特征向量进行民族判别,并通过Adam算法对网络进行优化,避免陷入局部最优值,添加正则化项保证算法稳定性;最后,分别采用2种网络结构进行对比实验,输入层、隐藏层和输出层的神经元个数分别为36、6、2和36、12、2,并设置不同初始学习率进行对比实验。结果表明:隐藏层神经元个数为12、学习率为0.000 1时,分类精度最高,测试阶段平均准确率最高为97.5%。为了验证所提方法的普适性,生成116例国外颅骨数据进行实验,测试阶段平均准确率为90.96%。相比较于支持向量机(SVM)、决策树、KNN、Fisher等机器学习方法,所提方法学习能力更强且分类精度有明显提升。 相似文献
767.
768.
盘腔积液现象在舰用燃气轮机工作过程中时有发生,汽化的滑油和水蒸气凝结形成积液。转子带动腔内的积液旋转,引发振动失稳,严重时会对发动机结构造成致命性破坏。为此,本文开展燃气轮机压气机盘腔积液的模拟实验研究,以双盘双支承的卧式柔性转子系统作为研究对象,重点关注小积液量的特点,对积液转子的动力学稳定性进行了研究。观测到转子的失稳现象,开展了不同积液体积、不同积液类型(水、植物油和滑油)等因素的影响规律研究,揭示了小积液的卧式转子动力学特征。研究结果表明:①对于积液失稳振动,存在失稳边界积液量,当积液量大于该边界值时,失稳将会发生。②失稳边界转速及恢复转速均高于临界转速。当转速高于失稳边界转速时,失稳将会发生。转速进一步增加,高于恢复转速时,失稳现象可能消失。③失稳时的振动特征为:出现幅值突增,次谐波成分也随之增加;基频和次谐波发生调制,表现出拍振特征。④随着积液体积的增加,失稳边界转速先减小后增加。⑤随着积液粘度系数增大,失稳边界转速和边界积液量均增大。 相似文献
770.