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A streamlined approach to hybrid-chemistry modeling for a low cetane-number alternative jet fuel

机译:低十六烷值替代喷气燃料的简化混合化学建模方法

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The development of renewable, alternative jet fuels presents an exigent challenge to the aviation community. In this work, a streamlined methodology for building computationally efficient kinetic models of real fuels from shock tube experiments is developed and applied to a low cetane-number, broad-boiling alternative jet fuel (termed C-4). A multi-wavelength laser absorption spectroscopy technique was used to determine species time-histories during the high-temperature pyrolysis of C-4, and a batch gradient descent optimization routine built a hybrid-chemistry (HyChem) kinetic model from the measured data. The model was evaluated using combustor-relevant, high-pressure ignition delay time measurements with satisfactory agreement. The present model enables predictive simulations of C-4 in practical environments, while the underlying methodology described here can be readily extended to build kinetic models for a broad range of real fuels of interest. (C) 2019 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:可再生的替代喷气燃料的发展对航空界提出了严峻的挑战。在这项工作中,开发了一种简化的方法,可通过冲击管实验建立计算有效的真实燃料动力学模型,并将其应用于低十六烷值,沸腾较大的代用喷气燃料(称为C-4)。使用多波长激光吸收光谱技术确定C-4高温热解过程中的物种时间历史,并且分批梯度下降优化例程从测量数据建立了杂化化学(HyChem)动力学模型。使用与燃烧室相关的高压点火延迟时间测量对模型进行了评估,结果令人满意。本模型可以在实际环境中对C-4进行预测性仿真,而此处描述的基本方法可以轻松扩展以建立适用于各种实际感兴趣的燃料的动力学模型。 (C)2019燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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