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Laminar flame speeds under engine-relevant conditions: Uncertainty quantification and minimization in spherically expanding flame experiments

机译:发动机相关条件下的层流火焰速度:球形膨胀火焰实验中的不确定性量化和最小化

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The spherically expanding flame method is the only approach for measuring laminar flame speeds at thermodynamic states that are relevant to engines. In the present study, a comprehensive evaluation of data obtained under constant pressure and constant volume conditions was carried out through experiments, development of a mathematically rigorous method for uncertainty quantification and propagation, and advancement of numerical models that describe the experiments accurately. The proposed uncertainty characterization approach accounts for parameters related to all measurements, data processing, and finally data interpretation. With the aid of direct numerical simulations, an alternative approach was proposed to derive laminar flame speeds in constant pressure experiments by eliminating the need for using extrapolation equations developed based on simplifying assumptions, which are known to be susceptible to major errors under certain conditions. The propagation of spherical flames under constant volume conditions was investigated through experiments carried out in an entirely spherical chamber and the use of two numerical models. The first involves the solution of the one-dimensional conservation equations of mass, species, and energy while accounting for pressure rise. The second model was developed based on thermodynamics similarly to existing literature, but radiation loss was introduced at the optically thin limit and approximations were made to allow for re-absorption with minimum computational cost. It was shown that neglecting radiation in constant volume experiments could introduce errors as high as 15%. Incorporating the aforementioned techniques, laminar flame speeds were measured and reported with properly quantified uncertainties for flames of synthesis gas for pressures ranging from 3 to 30 atm, and unburned mixture temperatures ranging from 298 to 550 K. Selected measurements were carried out as well for methane and propane flames for pressures ranging from 3 to 7 atm, and unburned mixture temperature of 298 K. The approaches introduced in this study allow for the determination of laminar flame speeds with notably reduced uncertainties under conditions of relevance to engines, which has major implications for the validation of kinetic models of surrogate and real fuels. (C) 2015 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:球形膨胀火焰法是在与发动机相关的热力学状态下测量层流火焰速度的唯一方法。在本研究中,通过实验对在恒定压力和恒定体积条件下获得的数据进行了综合评估,开发了数学上严格的不确定性量化和传播方法,并改进了精确描述实验的数值模型。所提出的不确定性表征方法考虑了与所有测量,数据处理以及最终数据解释相关的参数。借助于直接数值模拟,提出了一种替代方法,通过消除使用基于简化假设而开发的外推方程的需要来推导恒压实验中的层流火焰速度,而外推方程已知在某些条件下容易出现重大误差。通过在一个完全球形的室内进行实验并使用两个数值模型,研究了恒定体积条件下球形火焰的传播。首先涉及质量,物质和能量的一维守恒方程的求解,同时考虑了压力上升。第二种模型是根据与现有文献相似的热力学原理开发的,但是在光学上稀薄的极限处引入了辐射损耗,并进行了近似计算,以最小的计算成本实现了重新吸收。结果表明,在恒定体积实验中忽略辐射可能会导致高达15%的误差。结合上述技术,测量并记录了层流火焰速度,并适当量化了压力为3至30 atm,未燃烧混合物温度为298至550 K的合成气火焰的不确定性。还对甲烷进行了选定的测量丙烷火焰的压力范围为3至7个大气压,未燃烧的混合物温度为298K。本研究采用的方法可以确定层流火焰速度,在与发动机相关的条件下,不确定性显着降低,这对替代燃料和真实燃料动力学模型的验证。 (C)2015年燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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