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Development of a Quasi-Steady Approach Based Simulation Tool for System-Level Exhaust Aftertreatment Modelling

机译:基于准稳态仿真工具的开发用于系统级排气后处理建模的基于仿真工具

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This article describes a system-level 1D simulation tool that has been constructed on the Quasi-Steady (QS) method. By assuming that spatial changes are much greater than the temporal ones, rigorous 1D governing equations can be considerably simplified thus becoming less computationally demanding to solve and therefore suitable for control-oriented modelling purposes. With the proposed tool exhaust pipe wall temperature profiles, including multiple-wall-layer configurations, are solved through a finite difference scheme. Momentum equation is included for predicting pressure losses due to frictions and geometric irregularity. Exhaust fluid properties (transport and thermodynamic) are evaluated according to NASA or JANAF polynomial thermal data basis. The proposed tool allows the consideration of an arbitrary number of chemical species and reactions in the entire system. A novel semi-automatic approach was developed to handle catalytic reaction kinetics intuitively. Global reaction mechanisms and their rate formulations can be input or modified via a GUI system and, without any compiling requirements to generate a new executive command, are ready to use.
机译:本文介绍了在准稳态(QS)方法上构造的系统级1D仿真工具。通过假设空间变化远大于时间内,可以显着简化严格的1D控制方程,从而变得越来越苛刻,要求解决,因此适用于面向控制的建模目的。利用所提出的工具排气管壁温度曲线,包括多壁层配置,通过有限差分方案来解决。包括由于摩擦和几何不规则性导致的压力损失来包括动量方程。根据美国国家航空航天局或Janaf多项式热数据评价废液性质(传输和热力学)。所提出的工具允许考虑整个系统中的任意数量的化学物质和反应。开发了一种新型半自动方法,可直观地处理催化反应动力学。全局反应机制及其速率配方可以通过GUI系统输入或修改,而无需生成新的执行命令的任何编译要求即可使用。

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