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排序方式: 共有6619条查询结果,搜索用时 15 毫秒
1.
Alexander Van-Brunt Patrick E. Farrell Charles W. Monroe 《American Institute of Chemical Engineers》2022,68(5):e17599
We present the Onsager–Stefan–Maxwell thermodiffusion equations, which account for the Soret and Dufour effects in multicomponent fluids. Unlike transport laws derived from kinetic theory, this framework preserves the structure of the isothermal Stefan–Maxwell equations, separating the thermodynamic forces that drive diffusion from the force that drives heat flow. The Onsager–Stefan–Maxwell transport-coefficient matrix is symmetric, and the second law of thermodynamics imbues it with simple spectral characteristics. This new approach allows for heat to be considered as a pseudo-species and proves equivalent to both the intuitive extension of Fick's law and the generalized Stefan–Maxwell equations popularized by Bird, Stewart, and Lightfoot. A general inversion process facilitates the unique formulation of flux-explicit transport equations relative to any choice of convective reference velocity. Stefan–Maxwell diffusivities and thermal diffusion factors are tabulated for gaseous mixtures containing helium, argon, neon, krypton, and xenon. The framework is deployed to perform numerical simulations of steady three-dimensional thermodiffusion in a ternary gas. 相似文献
2.
约束矩阵方程组在振动理论、结构设计、系统辨识、数学控制理论、振动理论、地质学等诸多领域中有重要的应用价值.文章分析了矩阵方程组 , 对称解的迭代算法,使用该算法能够自动判断对称解的情况.当矩阵方程组相容时,能够得到矩阵方程组的对称解. 相似文献
3.
4.
针对大多数分数阶中立型随机时滞微分方程无法给出精确解的问题,给出了方程的一种数值解法.该方法首先将波形松弛方法推广到具有常延迟项的分数阶中立型随机微分方程,然后在分裂函数满足Lipschliz条件下证明了波形松弛方法在均方意义下收敛.数值模拟表明,波形松弛方法可用于求解分数阶中立型随机时滞微分方程. 相似文献
5.
Felipe A. Perdomo Siti H. Khalit Claire S. Adjiman Amparo Galindo George Jackson 《American Institute of Chemical Engineers》2021,67(3):e17194
The SAFT-γ Mie group-contribution equation of state is used to represent the fluid-phase behavior of aqueous solutions of a variety of linear, branched, and cyclic amines. New group interactions are developed in order to model the mixtures of interest, including the like and unlike interactions between alkyl primary, secondary, and tertiary amine groups (NH2, NH, N), cyclic secondary and tertiary amine groups (cNH, cN), and cyclic methine-amine groups (cCHNH, cCHN) with water (H2O). The group-interaction parameters are estimated from appropriate experimental thermodynamic data for pure amines and selected mixtures. By taking advantage of the group-contribution nature of the method, one can describe the fluid-phase behavior of mixtures of molecules comprising those groups over broad ranges of temperature, pressure, and composition. A number of aqueous solutions of amines are studied including linear, branched aliphatic, and cyclic amines. Liquid–liquid equilibria (LLE) bounded by lower critical solution temperatures (LCSTs) have been reported experimentally and are reproduced here with the SAFT-γ Mie approach. The main feature of the approach is the ability not only to represent accurately the experimental data employed in the parameter estimation, but also to predict the vapor–liquid, liquid–liquid, and vapor–liquid–liquid equilibria, and LCSTs with the same set of parameters. Pure compound and binary phase diagrams of diverse types of amines and their aqueous solutions are assessed in order to demonstrate the main features of the thermodynamic and fluid-phase behavior. 相似文献
6.
Hashim A.
Hashim 《国际强度与非线性控制杂志
》2020,30(10):3848-3870
》2020,30(10):3848-3870
This paper introduces two novel nonlinear stochastic attitude estimators developed on the Special Orthogonal Group with the tracking error of the normalized Euclidean distance meeting predefined transient and steady‐state characteristics. The tracking error is confined to initially start within a predetermined large set such that the transient performance is guaranteed to obey dynamically reducing boundaries and decrease smoothly and asymptotically to the origin in probability from almost any initial condition. The proposed estimators produce accurate attitude estimates with remarkable convergence properties using measurements obtained from low‐cost inertial measurement units. The estimators proposed in continuous form are complemented by their discrete versions for the implementation purposes. The simulation results illustrate the effectiveness and robustness of the proposed estimators against uncertain measurements and large initialization error, whether in continuous or discrete form. 相似文献
7.
对等通道转角挤压(ECAP)制备的超细晶纯钛,在温度为250~450 ℃、应变速率为10-5~1s-1的条件下进行热压缩实验。基于真应力和真应变实验数据,分别使用人工神经网络(ANN)和Arrhenius方程建立超细晶纯钛的热变形本构模型,研究其热变形行为。实验结果表明:在变形初期,流变应力随应变的增大而升高,随后趋于平缓,最终流变应力达到一个稳定值。人工神经网络训练和预测结果表明:人工神经网络最佳结构为3×12×1,人工神经网络模型预测的平均相对误差(AARE)为2.1%,相关系数(R)为0.9979,Arrhenius方程模型预测的AARE为11.54%,R为0.9464。即人工神经网络模型能够更加精确的描述超细晶纯钛的本构关系。通过对比不同温度下两种模型的误差,人工神经网络模型在高温条件下具有更好的稳定性。 相似文献
8.
Weiqiang Chen Jianhan Liang Xiaodong Cai Zhiyong Lin 《International Journal of Hydrogen Energy》2018,43(27):12460-12472
Adaptive simulations solving the Navier-Stokes equations have been conducted in order to get a better understanding on the detonation initiation and propagation in a stoichiometric H2/O2/Ar supersonic mixture with boundary layer. The detonation is initiated by a continuous hot jet. When reflecting on the wall, the jet induced bow shock interacts with the boundary layer and forms the shock boundary layer interaction phenomena, while in Euler result the bow shock forms Mach reflection. The investigation shows that the Navier-Stokes simulation result is structurally in better agreement with the experiment compared with that of the inviscid Euler simulation result. The bow shock interacts with the separation shock, forming the shock induced combustion behind the interaction zone. Then the combustion front couples with shock and forms Mach stem induced detonation. The Mach stem induced detonation continues to getting higher and propagating upstream, initiating the main flow. The initiated partial detonation exists with the separation shock induced combustion front, forming an “oblique shock induced combustion-partial detonation” structure in the main flow. The investigation on the influence of free stream Mach number further confirms that the boundary layer has an important influence on detonation initiation. The parametric studies also show that there exists a free stream Mach number range to initiate the partial detonation in supersonic combustible flow successfully. 相似文献
9.
ABSTRACTThis study investigates the use of numerical simulations to describe the solid-state diffusion of a sintering stage during a metal injection moulding process for micro-fluidic components with 316L stainless steel powders. Finite element (FE) analysis based on a thermo-elasto-viscoplastic model was conducted to describe the densification process of a stainless steel porous component during solid-state sintering. The numerical analyses, which were performed on a 3D micro-structured component with various powder volume loadings to take into account the thermal debinding effect to propose a full debinding sintering simulation, demonstrated that the FE simulation results are in agreement with the experimental ones. 相似文献
10.
Chahid Ayouch El-Hassan Essoufi Mouhcine Tilioua 《Computers & Mathematics with Applications》2019,77(5):1347-1357
The present paper deals with global existence of weak solutions of a time-space fractional Landau–Lifshitz–Bloch equation involving the weak Caputo derivative and a fractional Laplacian. We use Faedo–Galerkin method with some commutator estimates in order to prove global existence of weak solutions for the model. The uniqueness is also discussed in a special one dimensional case. 相似文献