正交各向异性平面弹性问题物性值V_(12)和G_(12)的反分析

采用边界元法和卡尔曼滤波对正交各向异性平面弹性问题物性值进行反分析,由有限个观测点的位移值反算出材料常数ν１２和 Ｇ１２．算例表明了该方法的有效性．     

铝合金Ly12尺寸稳定化处理工艺研究

本文重点介绍反淬火,高、低温循环处理工艺对Ly12合全的残余应力、显微组织、常规机械性能、微塑性变形抗力及尺寸稳定性的影响。同时,对高、低温循环处理工艺提高Ly12合金尺寸稳定性的机理进行了分析,确定了Ly12合金尺寸稳定化处理的优化工艺。     

飞行Ma12条件超燃发动机流场及燃烧特征分析

为提升针对高马赫数发动机的模拟能力,对计算方法进行了可压缩性修正,并针对飞行Ma12条件下超燃冲压发动机进行了多状态三维数值模拟,分析了发动机内波系、参数以及燃烧性能特征.研究结果表明:(1)修正后的方法计算所得激波位置及强度与试验值吻合,在激波串模拟、高马赫数发动机模拟上均展现了更优的能力.(2)发动机内形成激波与反...     

曲面拟合在拉格朗日反分析方法中应用的探讨

把一组不同位置的速度(应变)波形构筑的x-t域离散成8节点或9节点单元,每个单元的插值函数为10或12参数多项式,利用拉格朗日反分析可以得到相应的应力(速度)波形。正如路径线法,曲面拟合反分析的某一单元函数值计算需要利用前一单元与该单元交界点的计算值,因而误差生成和发展有时很难预测、控制。文中对不同位置、不同数量量计线情况下,拉格朗日反分析中的曲面拟合法及路径线法误差生成、发展进行了分析,分析结果对材料实验中布置速度(应变)传感器的数量及其间距是有一定帮助的。     

弹性、热弹性物性值反问题的边界元分析

本文采用边界元法和卡尔曼滤波,对弹性、热弹性问题物性值进行反分析,由有限个观测点的位移值,同时反算出材料的拉压弹性模量Ε、泊桑比ν和线膨胀系数α。     

预应力对LY12铝弹性前驱波的影响

通过过盈配合的热装配方法对LY12铝合金平面样品施加了径向预应力,采用平面飞片撞击方法获得了预应力对弹性前驱波的影响。结果表明:当飞片均以500 m/s的速度撞击样品时,压缩预应变为0(无预应变)、964.5×10-6和1 886.0×10-6时,弹性前驱波幅值分别为87.56、95.24、121.03 m/s,压缩预应力(变)提高了LY12铝弹性前驱波幅值。结合实验的特点,探讨了对样品施加静态径向预应力的数值模拟方法,结果表明,上升沿(100 μs)较为缓慢的加载可以达到与准静态加载应力分布一样的结果。采用该数值模拟方法给出和验证了弹性前驱波随压缩预应力增加而上升的计算结果,与实验结果较为吻合。     

弹性,热弹性物性值反问题的边界元分析

本文采用边界元法和卡尔曼滤波，对弹性，热弹性问题物性值进行反分析，由有限个点的位移值，同时反算出材料的拉压弹性模量Ｅ、泊桑比ｖ和线膨胀系数α。     

确定地基固结过程中材料参数的反分析法

结合有限单元法和数学规划法提出一确定地基固结过程中材料参数的反分析法。该法可以根据固结过程中的位移值和孔隙水压力值反算地基土的弹性系数、泊松比以及渗透系数。文中通过一些算例对该法进行了验证。     

基于后缘小翼的翼型反流动态失速主动控制试验研究

针对直升机旋翼反流区因反流动态失速导致的非定常载荷、阻力激增以及负升力等问题,开展了基于后缘小翼的翼型反流动态失速主动控制试验研究.采用动态压力测量结合翼型表面压力积分的方法,重点分析了后缘小翼不同的振荡相位差、幅值和减缩频率对反流动态失速控制的影响规律,对比了后缘小翼动态偏转和固定偏转的差异,试验雷诺数Re=3.5×10⁵.结果表明,当后缘小翼与翼型以相同的频率正弦振荡运动,且二者的相位差为0°时,能改善反流动态失速过程中钝几何前缘的流动分离,并在反流状态下实现了翼型负升力系数下降21.2%,阻力系数下降37.5%,俯仰力矩系数迟滞环面积下降44.6%的控制效果;动态偏转的后缘小翼对翼型反流动态失速的控制效果随后缘小翼振荡幅值的增加而增加,但进一步增加振荡幅值对于控制效果的提升有限;当减缩频率增加时,动态偏转的后缘小翼对反流状态下翼型阻力的控制效果会更加明显;后缘小翼的动态偏转与固定偏转都能有效改善翼型在反流中的动态气动性能,但是动态偏转对于不同翼型迎角的适应能力优于固定偏转,并取得了更好的非定常载荷控制以及更好的阻力和负升力改善效果.     

域外奇点法在弹性问题及其物性值反问题中的应用

本文采用域外奇点法中的位移法和应力法求解弹性问题，并对弹性物性值进行反分析，由有限个观测点的位移值。同时反算出材料的纵向弹性模量Ｅ和泊桑比Ｖ。本文方法属于边界型解法，可有效地避免解的奇异性，不需要数值积分，具有输入数据少，精度高，计算时间短和程序编制容易等优点。     

Influence of surface modification of SrFe12O19 particles with oleic acid on magnetic microsphere preparation

Oleic acid was used as surface modification agent to improve the hydrophobicity of magnetic strontium hexaferrite particles. The structure and properties of treated magnetic particles were characterized by scanning electronic microscopy （SEM）, Fourier transform infrared spectra （FTIR）, powder X-ray diffraction （XRD） and magnetic property measurement system （MPMS）. The results show that oleic acid is chemically enwrapped on the surface of SrFe12O19 particles. Magnetic particles modified by oleic acid are highly dispersible and strongly responsive to magnetism but with slight decrease in saturated magnetization. The affinity between magnetic particles and monomers is improved by surface modification, resulting in increased particle incorporation in magnetic polymeric microspheres. The surface modification mechanism of magnetic particles by oleic acid is addressed in this work.     

链子崖危岩体T8──T12缝段开裂变形机制的研究

文章通过对煤层采空区的分布、地压作用、山体开裂和近２０多年来的变形等方面的综合分析，得出链子崖危岩体具有南北强拉裂、东西弱拉裂和平面反时针转动的立体开裂变形机制。据此，作者进行了有针对性的计算，为危岩体综合加固体系的建立提供了依据。     

MoSi2-Mo5Si3-Mo5SiB2/SiC配对副的摩擦磨损性能

MoSi₂-Mo₅Si₃-Mo₅SiB₂复合材料是一种很有发展前景的高温耐磨材料，但MoSi₂-Mo₅Si₃-Mo₅SiB₂/SiC配对副的干滑动摩擦磨损性能尚不清楚. 本文中通过销-盘式干滑动摩擦磨损试验，考察了MoSi₂-Mo₅Si₃-Mo₅SiB₂/SiC配对副在不同温度(25~1 000 ℃)和载荷下(2.5~10 N)的摩擦学特性. 结果表明:试验温度和载荷对MoSi₂-Mo₅Si₃-Mo₅SiB₂/SiC配对副的摩擦系数影响较大，而对其磨损率影响较小. 载荷为5 N时，在25~1 000 ℃区间，摩擦系数和磨损率分别在0.11~0.43和0.513×10-7~0.544×10-7 mm3/(N·m)范围；在25~400 ℃时，磨损机制以轻微的氧化和黏着磨损为主，在600~1 000 ℃磨损机制主要表现为严重的氧化和黏着磨损. 在1 000 ℃时，随着载荷(2.5~10 N)的增加，摩擦系数和磨损率分别为0.29~0.38和0.540×10-7~0.547×10-7 mm3/(N·m)；载荷为2.5~10 N时，始终存在黏着和氧化磨损；载荷为7.5~10 N时，材料磨损表面还伴随碾压塑性变形的特征.      

Al0.2Co1.5CrFe1.2Ni1.5TiC0.4高熵合金的微观组织、力学与高温摩擦学性能

通过引入碳元素,设计了一种以原位形成的碳化物为增强相的高熵合金Al_(0.2)Co_(1.5)CrFe_(1.2)Ni_(1.5)TiC_(0.4),并采用放电等离子烧结(SPS)技术成功制备了这种高熵合金.采用XRD、SEM、EDS、万能材料试验机和高温摩擦磨损试验机等研究了微观组织、力学性能和室温至800℃下的摩擦学性能.结果表明:Al_(0.2)Co_(1.5)CrFe_(1.2)Ni_(1.5)TiC_(0.4)高熵合金由面心立方(FCC)结构的高熵固溶体基体相和弥散分布的TiC陶瓷相组成.FCC相使高熵合金具有良好的塑性和韧性,而TiC增强相赋予了高熵合金高的硬度和强度.随着温度的升高,高熵合金的摩擦系数和磨损率均具有逐渐减小的趋势.在800℃时,鉴于摩擦氧化作用,在磨损表面形成了致密的氧化物釉质层,起到了良好的减摩抗磨作用,使高熵合金表现出了优异的高温摩擦学性能.     

Exact solution of the non-linear differential equation RR̈ + 32R2 − AR−4 + B = 0

The non-linear equation $\text{R}\text{R}\text{?}\text{+}\text{3}\text{2}\text{R}{}^2\text{- AR}{}^{\mathrm{?4}}\text{+ B = 0}$ is shown to represent simply periodic motion with a minimum at R₁ and a maximum at R₁R₀ or a maximum at R₁ and a minimum at R₁R₀^?1. R₀ is a function of the ratio $\text{A}\text{B}$ and is greater than 1 for $\text{A}\text{B}$ > 1 and less than 1 for $\text{A}\text{B}$ > 1. The period of the motion satisfies the simple relation T(R₀^?1) = R₀^?1T(R₀). The exact solution to the above equation is represented in terms of elliptic integrals of the first and second kinds and a simple algebraic function.     

离子液体作为Si3N4-Ti3SiC2摩擦副润滑剂的摩擦学性能研究

采用SRV摩擦磨损试验机在室温及100 ℃下考察了两种离子液体（L-B106 和L-P106）、丙三醇、水作为Si₃N₄-Ti₃SiC₂摩擦副润滑剂的摩擦学行为,利用扫描电子显微镜（SEM）及X光电子能谱（XPS）对磨损表面进行了分析.结果表明：室温、20 N条件下,两种离子液体和丙三醇抗磨和减摩性能相当,室温、100 ℃条件下,L-P106相较于L-B106具有更好的润滑性能,且其抗磨和减摩性能均优于丙三醇,作为Si₃N₄-Ti₃SiC₂摩擦副润滑剂具有在苛刻环境条件下使用的应用前景. XPS分析结果表明：Ti₃SiC₂材料在摩擦过程中在摩擦热作用下生成了SiO_x、TiO₂,进而有效提高了Ti₃SiC₂摩擦副材料的抗磨损性能;此外,离子液体中的活性元素在Si₃N₄-Ti₃SiC₂摩擦副表面发生了复杂的摩擦化学反应,生成了由氟化钛、磷酸钛及硼酸钛等组成的具有减摩和抗磨性能的边界润滑膜.     

Structure cellulaire de la détonation des mélanges H2–NO2/N2O4Cellular structure of the detonation of gaseous mixtures H2–NO2/N2O4

Calculations of the detonation reaction zone of gaseous reactive mixtures of NO₂/N₂O₄ as oxidizer and H₂, CH₄ or C₂H₆ as fuel, in the range of equivalence ratio Φ between 0.5 and 2, show that, for Φ?1, the chemical energy is released in two distinct and successive exothermic steps with different chemical induction times. The first exothermic stage is mainly due to the reaction NO₂+H→NO+OH, NO being the main oxidizer of the second one.The experimental study conducted on the same range of equivalence ratio (0.5?Φ?2) shows that, for Φ?1, the detonation wave of these mixtures contains a double set of cellular structures. A similar result had already been obtained with the detonation of gaseous Nitromethane, the NO₂ group being here included in the molecule. Consequently, the oxidizer NO₂ being either initially separated from the fuel or included inside the molecule of a monopropellant (Nitromethane) is responsible, because of its specific chemical kinetics, of a chemical energy release in two main steps and of the existence of a double cellular structure in the detonation wave for the same range of equivalence ratio. These results reinforce the assumption that the cellular structure of the detonation finds its origin in the strong rates of chemical energy release inside the reaction zone. To cite this article: F. Joubert et al., C. R. Mecanique 331 (2003).     

Measurement of the concentration diffusion coefficient for Ne-Ar, Ne-Xe, Ne-H2, Xe-H2, H2-N2 and H2-O2 gas systems

The concentration diffusion coefficient, D ₁₂, is measured for the equimolar mixtures of Ne-Ar, Ne-Xe, Ne-H₂, Xe-H₂, H₂-N₂ and H₂-O₂ binary gas systems in a two-bulb metal apparatus in the temperature range 0 C to 100 C. These values are compared with the existing data on these systems and with the predictions of the kinetic theory in conjunction with the modified Buckingham exp-six potential. Unlike the thermal diffusion coefficient, with the simple theory it is possible to predict D ₁₂ within a few percent even for systems involving polyatomic gases. The smoothed experimental D ₁₂ values are also used to obtain data for the coefficients of viscosity and thermal conductivity at round temperatures and compositions for these systems.Nomenclature C ₂ ^t relative amount of a gas in the mixture in the bulb 2 at an instant t - C ₂ relative amount of the same gas in the mixture in the bulb 2 at equilibrium - D ₁₂ diffusion coefficient - X ₁ mole-fraction of the heavier component in the mixture - _mix viscosity coefficient - _mix thermal conductivity coefficient     

Kinetics of ultrafine coating of SiO2 nanoparticles, suspended in non-thermal CH4/C2H6 plasma

Capacitively coupled RF discharges in methane and ethane (1000–3000 Pa, 5–15 W/cm³) were used for the in-flight coating of SiO₂ nanopowders (NP) with an a-C:H layer [A. Kouprine, F. Gitzhofer, M. Boulos, A. Fridman, Polymer-like C:H thin film coating of nanopowders in capacitively coupled RF discharge, Plasma Chemistry and Plasma Processing 24 (2) (2004) 189–215]. In this present work a model of the chemical kinetics of this plasma processing has been developed, based on the GRI-Mech 3.0 mechanism [G.P. Smith, D.M. Golden, M. Frenklach, Gas Research Institute, Detailed chemical reaction mechanism. Available from: ], and calculations are performed, using the Chemkin-II code. The model includes the formation of two solid phases: an amorphous C:H coating, deposited on the suspended NP, and soot, incepted in the gas phase. Non-equilibrium plasma effects are taken into account by the rates of radical species’ production, using the reference data on the “G-value”. The CH₃ and H species appear to have key roles in surface activation and the nanofilm growth. The results demonstrate the competitive character of the formation of the two solid phases: the C:H coating is dominant under T_gas < 1400–1600 K, depending on the conditions, and soot commencing to dominate at higher temperatures. This division corresponds to the passage from non-thermal plasma conditions, with the dominance of single-valent radicals and solid phase growth on the substrate only, to the plasma thermalisation with the formation of two-valent radicals and v. inception of the solid phase. The results are validated experimentally by the observation of soot formation as a function of the gas temperature, by the mass spectrograph data on the gas composition after plasma reforming, and by the reference data on coating growth rates and induction times for soot formation.