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Response mapping methodology for premixed systems.

机译:预混系统的响应映射方法。

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Practical combustion systems like gas turbines and internal combustion engines involve non-equilibrium chemistry. Numerical solution for such equations is tedious and involves solution of conservation and chemistry equations concurrently. A simpler approach is sought. Response modeling is one such technique. It involves pre-integrating the chemistry information and making it available to the physical system. The method reduces the stiffness of the equations, while maintaining the non-equilibrium information.; Premixed system while simple to model captures the complexities of a real combustion systems. Developing a method for using a response model for such a system is the goal of the present work. Propane is an hydrocarbon which exhibits properties similar to heavier molecules like gasoline. It is also a commonly used fuel. Moreover the reaction set for propane is manageable for purposes of integration. Hence, propane-air combustion is chosen for simulations.; A zero dimensional model representing a fluid particle traveling in a premix space while receiving energy fluxes is developed. The zero-dimensional solution from the model captures all the essential physics of a 1D premix combustion. Modifying the two key parameters in the model gives us wide range of solutions to different initial conditions.; Fifty-six simulations with different initial conditions are run. The information is used for mapping. The mapping procedure calls for certain parameters be mapped directly with neural networks while parameterizing others into profile shape for implementation. All the key variables necessary for developing the response model are obtained from the pre-integrated set.; Modified one-dimensional premix equations without the species fluxes are solved with the response map. The equation set is reduced to two first order ordinary differential equations and integrated by a fourth order Runge-Kutta method. Results are compared for different cases.
机译:诸如燃气轮机和内燃机的实用燃烧系统涉及非平衡化学。这些方程的数值解很繁琐,同时涉及到守恒和化学方程的解。寻求一种更简单的方法。响应建模就是这样一种技术。它涉及预先整合化学信息并将其提供给物理系统。该方法降低了方程的刚度,同时保持了非平衡信息。预混系统虽然易于建模,却可以捕捉到实际燃烧系统的复杂性。开发一种用于这种系统的响应模型的方法是本工作的目标。丙烷是一种碳氢化合物,具有类似于汽油等重分子的特性。它也是一种常用的燃料。此外,出于整合的目的,丙烷的反应组是可控制的。因此,选择丙烷-空气燃烧进行模拟。建立了一个零维模型,该模型表示在接收能量通量的同时在预混空间中传播的流体粒子。该模型的零维解捕获了一维预混燃烧的所有基本物理原理。修改模型中的两个关键参数为我们提供了针对不同初始条件的广泛解决方案。使用不同的初始条件进行了56次仿真。该信息用于映射。映射过程要求将某些参数直接与神经网络映射,同时将其他参数参数化为轮廓形状以实现。开发响应模型所需的所有关键变量均从预集成集中获得。修改后的一维预混方程,没有物质通量,可以通过响应图求解。该方程组简化为两个一阶常微分方程,并通过四阶Runge-Kutta方法进行积分。比较不同情况下的结果。

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